Movable Object For Performing Real-time Mapping

Abstract

Techniques are disclosed for real-time mapping in a movable object environment. A real-time mapping system can include at least an unmanned aerial vehicle (UAV), comprising a propulsion system, a main body coupled to the propulsion system and a payload assembly coupled to the main body via a mounting assembly, wherein the payload assembly includes a payload comprising a scanning sensor and a positioning sensor, the payload assembly configured to orient the scanning sensor at a plurality of angles relative to the main body.

Description

CROSS-REFERENCE TO RELATED APPLICATIONS

[0001] This application is a continuation of International Patent Application No. PCT/US2019/058219, filed Oct. 25, 2019, which claims the benefit of U.S. Provisional Application No. 62/752,273, filed Oct. 29, 2018, which is hereby incorporated by reference.

COPYRIGHT NOTICE

[0002] A portion of the disclosure of this patent document contains material which is subject to copyright protection. The copyright owner has no objection to the facsimile reproduction by anyone of the patent document or the patent disclosure, as it appears in the Patent and Trademark Office patent file or records, but otherwise reserves all copyright rights whatsoever.

FIELD OF THE INVENTION

[0003] The disclosed embodiments relate generally to techniques for mapping and more particularly, but not exclusively, to a movable object for performing real-time mapping.

BACKGROUND

[0004] Movable objects such as unmanned aerial vehicles (UAVs) can be used for performing surveillance, reconnaissance, and exploration tasks for various applications. Movable objects may carry a payload, including various sensors, which enables the movable objects to capture sensor data during movement of the movable objects. The captured sensor data may be rendered on a client device, such as a client device in communication with the movable objects via a remote control, remote server, or other computing device.

SUMMARY

[0005] Techniques are disclosed for real-time mapping in a movable object environment. A real-time mapping system can include at least an unmanned aerial vehicle (UAV), comprising a propulsion system, a main body coupled to the propulsion system and a payload assembly coupled to the main body via a mounting assembly, wherein the payload assembly includes a payload comprising a scanning sensor and a positioning sensor, the payload assembly configured to orient the scanning sensor at a plurality of angles relative to the main body.

BRIEF DESCRIPTION OF DRAWINGS

[0006] FIG. 1 illustrates an example of a movable object in a movable object environment, in accordance with various embodiments.

[0007] FIG. 2 illustrates an example of a movable object architecture in a movable object environment, in accordance with various embodiments.

[0008] FIG. 3 illustrates an example of a mapping manager in a movable object environment, in accordance with various embodiments.

[0009] FIGS. 4A and 4B illustrate an example of a hierarchical data structure, in accordance with various embodiments.

[0010] FIGS. 5A and 5B illustrate an example of outlier removal in mapping data, in accordance with various embodiments.

[0011] FIG. 6 illustrates an example of intensity values in mapping data, in accordance with various embodiments.

[0012] FIG. 7 illustrates an example of supporting a movable object interface in a software development environment, in accordance with various embodiments.

[0013] FIG. 8 illustrates an example of a movable object interface, in accordance with various embodiments.

[0014] FIG. 9 illustrates an example of components for a movable object in a software development kit (SDK), in accordance with various embodiments.

[0015] FIG. 10 shows a flowchart of a method of target mapping in a movable object environment, in accordance with various embodiments.

[0016] FIG. 11 shows an isometric view of a movable object for performing real-time mapping, in accordance with an embodiment.

[0017] FIG. 12 shows a rear view of a movable object for performing real-time mapping, in accordance with an embodiment.

[0018] FIG. 13 shows an isometric exploded view of the mounting assembly and payload assembly, in accordance with an embodiment.

[0019] FIG. 14 shows an isometric view of base plate, in accordance with some embodiments.

[0020] FIG. 15 shows an isometric assembled view of the mounting assembly and payload assembly, in accordance with an embodiment.

[0021] FIGS. 16A-16D show additional views of the payload assembly in accordance with various embodiments.

[0022] FIG. 17 shows an alternative enclosure to prevent jamming of the positioning sensor of a movable object in accordance with various embodiments.

[0023] FIGS. 18A and 18B show example alignments of lower expansion brackets in accordance with various embodiments.

[0024] FIG. 19 shows an example of the alignment brackets being connected to the movable object body and the expansion brackets, in accordance with an embodiment.

[0025] FIG. 20 shows an alternative mechanical attachment of the payload assembly to a movable object in accordance with various embodiments.

[0026] FIGS. 21-23 show an alternative mechanical attachment of the light detection and ranging (LiDAR) sensor and positioning sensor to a movable object in accordance with various embodiments.

[0027] FIG. 24 shows an example of a landing gear in accordance with various embodiments.

[0028] FIG. 25 shows an example of a landing gear bracket in accordance with various embodiments.

[0029] FIG. 26 shows an example of an alternative landing gear mounting point in accordance with various embodiments.

[0030] FIGS. 27-29 show LiDAR fields of view in accordance with various embodiments.

[0031] FIGS. 30-32 show examples of angled positions of a scanning sensor coupled to a movable object, in accordance with various embodiments.

[0032] FIG. 33 shows example scanning patterns that may be implemented by LiDAR sensors that may be used in various embodiments.

DETAILED DESCRIPTION

[0033] The invention is illustrated, by way of example and not by way of limitation, in the figures of the accompanying drawings in which like references indicate similar elements. It should be noted that references to "an" or "one" or "some" embodiment(s) in this disclosure are not necessarily to the same embodiment, and such references mean at least one.

[0034] The following description of the invention describes target mapping using a movable object. For simplicity of explanation, an unmanned aerial vehicle (UAV) is generally used as an example of a movable object. It will be apparent to those skilled in the art that other types of movable objects can be used without limitation.

[0035] Embodiments enable a movable object to map a target environment in real-time using data collected from a positioning sensor and a scanning sensor. Alternative embodiments may take advantage of post-processing to generate a map following completion of one or more data collection missions executed by one or more movable objects. For example, the various embodiments may utilize scan matching techniques for mapping a complex target environment. Embodiments can be used to provide LiDAR-based real-time mapping for various applications, such as construction, surveying, target inspection, etc. Rather than collecting data to be post-processed into a map representation of the target, a map can be constructed in real-time, enabling a version of the map to be rendered on a client device as it is collected. Such live rendering may enable the user to determine if any areas within the target environment have not been scanned by a scanning sensor electronically coupled to the movable object. Additionally, a high-density version of the map can be generated during the mapping mission and downloaded upon return of the movable object. In various embodiments, a mapping manager may utilize a parallel computing architecture to perform the real-time mapping while the movable object is performing its mapping mission. In some embodiments, the mapping data may be output as a LiDAR Data Exchange File (LAS) which may be used by various tools to render the map of the target environment and/or use the mapping data for further processing, planning, etc. Metadata embedded in the LAS output file can facilitate integration of the map with various third-party tools. In various embodiments, the map may be output in various file formats depending on user preferences.

[0036] In some embodiments, a mapping manager can receive mapping data from a scanning sensor (such as a LiDAR sensor or other sensor that provides high resolution scanning of a target environment), and positioning data from a positioning sensor (e.g., a global positioning system (GPS) module, real-time kinematic (RTK) module, an inertial measurement unit (IMU) module, or other positioning sensor). The mapping data can be geo-referenced using the positioning data and used to construct the map of the target environment. Embodiments objectively geo-reference the mapping data, enabling various target environments to be mapped regardless of environment complexity.

[0037] FIG. 1 illustrates an example of a movable object in a movable object environment 100, in accordance with various embodiments. As shown in FIG. 1, client device 110 in a movable object environment 100 can communicate with a movable object 104 via a communication link 106. The movable object 104 can be an unmanned aircraft, an unmanned vehicle, a handheld device, and/or a robot. The client device 110 can be a portable personal computing device, a smart phone, a remote control, a wearable computer, a virtual reality/augmented reality system, and/or a personal computer. Additionally, the client device 110 can include a remote controller 111 and communication system 120A, which is responsible for handling the communication between the client device 110 and the movable object 104 via communication system 120B. For example, the communication between the client device 110 and the movable object 104 (e.g., an unmanned aircraft) can include uplink and downlink communication. The uplink communication can be used for transmitting control signals, the downlink communication can be used for transmitting media or video stream, mapping data collected scanning sensors, or other sensor data collected by other sensors.

[0038] In accordance with various embodiments, the communication link 106 can be (part of) a network, which is based on various wireless technologies, such as the WiFi, Bluetooth, 3G/4G, and other radio frequency technologies. Furthermore, the communication link 106 can be based on other computer network technologies, such as the internet technology, or any other wired or wireless networking technology. In some embodiments, the communication link 106 may be a non-network technology, including direct point-to-point connections such as universal serial bus (USB) or universal asynchronous receiver-transmitter (UART).

[0039] In various embodiments, movable object 104 in a movable object environment 100 can include a payload assembly 122 and a payload, such as a scanning sensor 124 (e.g., a LiDAR sensor). Although the movable object 104 is described generally as an aircraft, this is not intended to be limiting, and any suitable type of movable object can be used. One of skill in the art would appreciate that any of the embodiments described herein in the context of aircraft systems can be applied to any suitable movable object (e.g., a UAV). In some instances, the payload may be provided on the movable object 104 without requiring the payload assembly.

[0040] In accordance with various embodiments, the movable object 104 may include one or more movement mechanisms 116 (e.g., propulsion mechanisms), a sensing system 118, and a communication system 120B. The movement mechanisms 116 can include one or more of rotors, propellers, blades, engines, motors, wheels, axles, magnets, nozzles, animals, or human beings. For example, the movable object may have one or more propulsion mechanisms. The movement mechanisms may all be of the same type. Alternatively, the movement mechanisms can be different types of movement mechanisms. The movement mechanisms 116 can be mounted on the movable object 104 (or vice-versa), using any suitable means such as a support element (e.g., a drive shaft). The movement mechanisms 116 can be mounted on any suitable portion of the movable object 104, such on the top, bottom, front, back, sides, or suitable combinations thereof.

[0041] In some embodiments, the movement mechanisms 116 can enable the movable object 104 to take off vertically from a surface or land vertically on a surface without requiring any horizontal movement of the movable object 104 (e.g., without traveling down a runway). Optionally, the movement mechanisms 116 can be operable to permit the movable object 104 to hover in the air at a specified position and/or orientation. One or more of the movement mechanisms 116 may be controlled independently of the other movement mechanisms, for example by an application executing on client device 110, computing device 112, or other computing device in communication with the movement mechanisms. Alternatively, the movement mechanisms 116 can be configured to be controlled simultaneously. For example, the movable object 104 can have multiple horizontally oriented rotors that can provide lift and/or thrust to the movable object. The multiple horizontally oriented rotors can be actuated to provide vertical takeoff, vertical landing, and hovering capabilities to the movable object 104. In some embodiments, one or more of the horizontally oriented rotors may spin in a clockwise direction, while one or more of the horizontally oriented rotors may spin in a counterclockwise direction. For example, the number of clockwise rotors may be equal to the number of counterclockwise rotors. The rotation rate of each of the horizontally oriented rotors can be varied independently in order to control the lift and/or thrust produced by each rotor, and thereby adjust the spatial disposition, velocity, and/or acceleration of the movable object 104 (e.g., with respect to up to three degrees of translation and up to three degrees of rotation). As discussed further herein, a controller, such as flight controller 114, can send movement commands to the movement mechanisms 116 to control the movement of movable object 104. These movement commands may be based on and/or derived from instructions received from client device 110, computing device 112, or other entity.

[0042] The sensing system 118 can include one or more sensors that may sense the spatial disposition, velocity, and/or acceleration of the movable object 104 (e.g., with respect to various degrees of translation and various degrees of rotation). The one or more sensors can include any of the sensors, including GPS sensors, motion sensors, inertial sensors, proximity sensors, or image sensors. The sensing data provided by the sensing system 118 can be used to control the spatial disposition, velocity, and/or orientation of the movable object 104 (e.g., using a suitable processing unit and/or control module). Alternatively, the sensing system 118 can be used to provide data regarding the environment surrounding the movable object, such as weather conditions, proximity to potential obstacles, location of geographical features, location of manmade structures, and the like.

[0043] The communication system 120B enables communication with client device 110 via communication link 106, which may include various wired and/or wireless technologies as discussed above, and communication system 120A. The communication system 120A or 120B may include any number of transmitters, receivers, and/or transceivers suitable for wireless communication. The communication may be one-way communication, such that data can be transmitted in only one direction. For example, one-way communication may involve only the movable object 104 transmitting data to the client device 110, or vice-versa. The data may be transmitted from one or more transmitters of the communication system 120B of the movable object to one or more receivers of the communication system 120A of the client device, or vice-versa. Alternatively, the communication may be two-way communication, such that data can be transmitted in both directions between the movable object 104 and the client device 110. The two-way communication can involve transmitting data from one or more transmitters of the communication system 120B of the movable object 104 to one or more receivers of the communication system 120A of the client device 110, and transmitting data from one or more transmitters of the communication system 120A of the client device 110 to one or more receivers of the communication system 120B of the movable object 104.

[0044] In some embodiments, a client device 110 may communicate with a mapping manager 126 installed on computing device 112 over a transparent transmission channel of a communication link 106. The transparent transmission channel can be provided through the flight controller of the movable object which allows the data to pass through unchanged (e.g., "transparent") to the mapping manager or other application on computing device 112. In some embodiments, mapping manager 126 may utilize a software development kit (SDK), application programming interfaces (APIs), or other interfaces made available by the movable object, computing device, scanning sensor 124, etc. In various embodiments, the mapping manager may be implemented by one or more processors on movable object 104 (e.g., flight controller 114 or other processors), computing device 112, remote controller 111, client device 110, or other computing device in communication with movable object 104. In some embodiments, mapping manager 126 may be implemented as an application executing on client device 110, computing device 112, or other computing device in communication with movable object 104.

[0045] In some embodiments, an application executing on client device 110 or computing device 112 can provide control data to one or more of the movable object 104, payload assembly 122, and payload 124 and receive information from one or more of the movable object 104, payload assembly 122, and payload 124 (e.g., position and/or motion information of the movable object, payload assembly or payload; data sensed by the payload such as image data captured by a payload camera or mapping data captured by a LiDAR sensor; and data generated from image data captured by the payload camera or LiDAR data generated from mapping data captured by the LiDAR sensor).

[0046] In some embodiments, the control data may result in a modification of the location and/or orientation of the movable object (e.g., via control of the movement mechanisms 116), or a movement of the payload with respect to the movable object (e.g., via control of the payload assembly 122). The control data from the application may result in control of the payload, such as control of the operation of scanning sensor 124, a camera or other image capturing device (e.g., taking still or moving pictures, zooming in or out, turning on or off, switching imaging modes, changing image resolution, changing focus, changing depth of field, changing exposure time, changing viewing angle or field of view).

[0047] In some instances, the communications from the movable object, payload assembly and/or payload may include information obtained from one or more sensors (e.g., of the sensing system 118 or of the scanning sensor 124 or other payload) and/or data generated based on the sensing information. The communications may include sensed information obtained from one or more different types of sensors (e.g., GPS sensors, motion sensors, inertial sensors, proximity sensors, or image sensors). Such information may pertain to the position (e.g., location, orientation), movement, or acceleration of the movable object, payload assembly, and/or payload. Such information from a payload may include data captured by the payload or a sensed state of the payload.

[0048] In some embodiments, computing device 112 can be added to the movable object. The computing device can be powered by the movable object and can include one or more processors, such as CPUs, GPUs, field programmable gate arrays (FPGAs), system on chip (SoC), application-specific integrated circuit (ASIC), or other processors. The computing device can include an operating system (OS), such as Windows 10.RTM., Linux.RTM., Unix.RTM.-based operating systems, or other OS. Mission processing can be offloaded from the flight controller 114 to the computing device 112. In various embodiments, the mapping manager 126 can execute on the computing device 112, client device 110, payload 124, a remote server (not shown), or other computing device.

[0049] In some embodiments, mapping manager 126 can be used to provide LiDAR-based real-time mapping for various applications, such as construction, surveying, target inspection, etc. Rather than collecting data to be post-processed into a map representation of the target, a map can be constructed in real-time, enabling a version of the map to be rendered on client device 110 as it is collected. Such live rendering may enable the user to determine if any areas within the target environment have not been scanned by scanning sensor 124. Additionally, another version of the map may be downloaded and used upon return of the movable object. In various embodiments, the mapping manager 126 may utilize a parallel computing architecture in computing device 112 to perform the real-time mapping. In some embodiments, the mapping manager 126 may perform data compression to transform a dense map into a sparse map to be rendered on client device 110. By way of compressing the dense map into the sparse map, the mapping manager 126 may be used to reduce data size required for transmission from the movable object 104 to the client device 110, and thus, data transmission time and bandwidth are saved for efficient real-time map rendering. In such embodiments, the live rendering of the map may be a lower resolution or a compressed data version of the map (i.e., a sparse map) compared to the version obtained from the movable object upon its return from scanning the target environment (i.e., a dense map). In some embodiments, the map may be output as a LiDAR Data Exchange File (LAS) which may be used by various tools to render the map of the target environment and/or use the mapping data for further processing, planning, etc. Metadata embedded in the LAS output file can facilitate integration of the map with various third-party tools. In various embodiments, the map may be output in various file formats depending on user preferences.

[0050] Mapping manager 126 can receive mapping data from scanning sensor 124. As discussed, scanning sensor 124 may be a LiDAR sensor or other sensor that provides high resolution scanning of a target environment. The mapping manager 126 may also receive positioning data from a positioning sensor (e.g., a GPS module, RTK module, or other positioning sensor). In some embodiments, the positioning sensor may be part of functional modules 108, sensing system 118, or a separate module coupled to movable object 104 which provides positioning data for the movable object. The mapping data can be geo-referenced using the positioning data and used to construct the map of the target environment. Prior methods of 3D mapping have relied on complex environments that are conducive to scan-matching. Unlike prior mapping systems, which require complex environments in order to use scan-matching to prepare the map, embodiments objectively geo-reference the mapping data. This allows for various target environments to be mapped regardless of environment complexity.

[0051] Additional details of the movable object architecture are described below with respect to FIG. 2.

[0052] FIG. 2 illustrates an example 200 of a movable object architecture in a movable object environment, in accordance with various embodiments. As shown in FIG. 2, a movable object 104 can include a computing device 112 and flight controller 114. The computing device 112 can connect to the scanning sensor 124 via a high bandwidth connection, such as Ethernet or universal serial bus (USB). The computing device 112 may also connect to a positioning sensor 202 over a low bandwidth connection, such as universal asynchronous receiver-transmitter (UART). As discussed, the positioning sensor 202 may be included as a separate module (as shown in FIG. 2) or may be included as part of functional modules 108 or sensing system 118. Positioning sensor 202 may include a radio 204, such as a 4G, 5G, or other cellular or mobile network radio. The radio 204 may be used by RTK module 206 to enhance positioning data collected by GPS module 208. Although a GPS module is shown in FIG. 2, any global navigation satellite service may be used, such as GLOSNASS, Galileo, BeiDou, etc. RTK module 206 can receive a reference signal from a reference station using radio 204 and provide a correction to the positioning data provided by GPS module 208. Additionally, GPS module 208 can output a clock signal, such as a pulse per second (1PPS) signal, to the scanning sensor 124. This allows for the scanning sensor and the GPS sensor to apply synchronized time stamps to their collected data using the same clock signal.

[0053] In various embodiments, the computing device 112 can connect to one or more high bandwidth components, such as one or more cameras, a stereo vision module, or payload. The computing device 112 can connect to the flight controller 114 via UART and/or USB to send and receive data to and from the remote control via communication system 120B. In various embodiments, the computing device 112 may include one or more CPUs, GPUs, field programmable gate arrays (FPGA), systems on chip (SoC), or other processor(s).

[0054] Flight controller 114 can connect to various functional modules 108, such as magnetometer 210, barometer 212, and inertial measurement unit (IMU) 214. In some embodiments, communication system 120B can connect to computing device 112 instead of, or in addition to, flight controller 114. In some embodiments, sensor data collected by the one or more functional modules 108 and the positioning sensor 202 can be passed from the flight controller 114 to the computing device 112.

[0055] In some embodiments, flight controller 114 and computing device 112 can be implemented as separate devices (e.g., separate processors on separate circuit boards). Alternatively, one or more of the flight controller 114 and computing device 112 can be implemented as a single device, such as an SoC. In various embodiments, computing device 112 may be removable from the movable object.

[0056] FIG. 3 illustrates an example 300 of a mapping manager 126 in a movable object environment, in accordance with various embodiments. As shown in FIG. 3, a mapping manager 126 may execute on one or more processors 302 of computing device 112. The one or more processors 302 may include CPUs, GPUs, FGPAs, SoCs, or other processors, and may be part of a parallel computing architecture implemented by computing device 112. The mapping manager 126 may include sensor interfaces 303, data preparation module 308, and map generator 316.

[0057] Sensor interfaces 303 can include a scanning sensor interface 304 and a positioning sensor interface 306. The sensor interfaces 303 may include hardware and/or software interfaces. The scanning sensor interface 304 can receive data from the scanning sensor (e.g., a LiDAR or other scanning sensor) and the positioning sensor interface 306 can receive data from the positioning sensor (e.g., a GPS sensor, an RTK sensor, an IMU sensor, and/or other positioning sensors or a combination thereof). In various embodiments, the scanning sensor may produce mapping data in a point cloud format. The point cloud of the mapping data may be a three-dimensional representation of the target environment. In some embodiments, the point cloud of the mapping data may be converted to a matrix representation. The positioning data may include GPS coordinates for the movable object and, in some embodiments, may include roll, pitch, and yaw values associated with the movable object corresponding to each GPS coordinate. The roll, pitch, and yaw values may be obtained from the positioning sensor, such as an inertial measurement unit (IMU), or other sensor. As discussed, the positioning data may be obtained from an RTK module, which corrects the GPS coordinates based on a correction signal received from a reference station. In some embodiments, the RTK module may produce a variance value associated with each output coordinate. The variance value may represent the accuracy of the corresponding positioning data. For example, if the movable object is performing sharp movements, the variance value may go up, indicating less accurate positioning data has been collected. The variance value may also vary depending on atmospheric conditions, leading to different accuracies measured by the movable object depending on the particular conditions present when the data was collected.

[0058] The positioning sensor and scanning sensor may share clock circuitry. For example, the positioning sensor may include clock circuitry and output a clock signal to the scanning sensor. In some embodiments, a separate clock circuit may output a clock signal to both the scanning sensor and the positioning sensor. As such, the positioning data and the mapping data may be time-stamped using the shared clock signal.

[0059] In some embodiments, the positioning sensor and scanning sensor may output data with differing delays. For example, the positioning sensor and the scanning sensor may not start generating data at the same time. As such, the positioning data and/or mapping data may be buffered to account for the delay. In some embodiments, a buffer size may be chosen based on the delay between the output of each sensor. In some embodiments, mapping manager can receive the data from the positioning sensor and scanning sensor and output synchronized data using the timestamps shared by the sensor data with respect to the shared clock signal. This enables the positioning data and mapping data to be synchronized before further processing. Additionally, the frequency of the data obtained from each sensor may be different. For example, the scanning sensor may be producing data in the range of hundreds of kHz, while the positioning sensor may be producing data in the range of hundreds of Hz. Accordingly, to ensure each point of the mapping data has corresponding positioning data, upsampling module 310 can interpolate the lower frequency data to match the higher frequency data. For example, assuming the positioning data is produced by the positioning sensor at 100 Hz and the mapping data is produced by the scanning sensor (e.g., a LiDAR sensor) at 100 kHz, the positioning data may be upsampled from 100 Hz to 100 kHz. Various upsampling techniques may be used to upsample the positioning data. For example, a linear fit algorithm, such as least squares, may be used. In some embodiments, non-linear fit algorithms may be used to upsample the positioning data. Additionally, the roll, pitch, yaw values of the positioning data may also be interpolated to match the frequency of the mapping data. In some embodiments, the roll, pitch, and yaw values may be spherical linear interpolated (SLERP) to match the number of points in the mapping data. The time stamps may likewise be interpolated to match the interpolated positioning data.

[0060] Once the positioning data has been upsampled and synchronized with the mapping data by upsampling module 310, geo-reference module 312 can convert the matrix representation of the mapping data from the frame of reference (or the reference coordinate system) in which it was collected (e.g., scanner reference frame or scanner reference coordinate system) to a desired frame of reference (or a desired reference coordinate system). For example, the positioning data may be converted from the scanner reference frame to a north-east-down (NED) reference frame (or a NED coordinate system). The reference frame to which the positioning data is converted may vary depending on the application of the map that is being produced. For example, if the map is being used in surveying, it may be converted to the NED reference frame. For another example, if the map is being used for rendering motions such as flight simulation, it may be converted to the FlightGear coordinate system. Other applications of the map may effect conversions of the positioning data to different reference frames or different coordinate systems.

[0061] Each point in the point cloud of the mapping data is associated with a position in the scanner reference frame that is determined relative to the scanning sensor. The positioning data of the movable object, produced by the positioning sensor, may then be used to convert this position in the scanner reference frame to the output reference frame in a world coordinate system, such as a GPS coordinate system. For example, the position of the scanning sensor in the world coordinate system is known based on the positioning data. In some embodiments, the positioning sensor and the scanning module may be offset (e.g., due to being located at different positions on the movable object). In such embodiments, a further correction factoring in this offset may be used to convert from the scanner reference frame to the output reference frame (e.g., each measured position in the positioning data may be corrected using the offset between the positioning sensor and the scanning sensor). For each point in the point cloud of the mapping data, the corresponding positioning data can be identified using the time stamp. The point can then be converted to the new reference frame. In some embodiments, the scanner reference frame can be converted into a horizontal reference frame using the interpolated roll, pitch, and yaw values from the positioning data. Once the mapping data has been converted into the horizontal reference frame, it may be further converted into a Cartesian frame or other output reference frame. Once each point has been converted, the result is a geo-referenced point cloud, with each point in the point cloud now referenced to the world coordinate system. In some embodiments, the geo-referenced point cloud can be provided to map generator 316 before performing outlier removal to remove outlier data from the geo-referenced point cloud.

[0062] After the geo-referenced point cloud has been produced, outlier removal module 314 can remove outlier data from the geo-referenced point cloud. In some embodiments, the geo-referenced point cloud may be downsampled, reducing the number of outliers in the data. Downsampling of this data may be performed using voxels. In some embodiments, the points in each voxel may be averaged, and one or more averaged points may be output per voxel. As such, outlier points will be removed from the data set in the course of averaging the points in each voxel. In various embodiments, the resolution of the voxels (e.g., the size of each voxel), may be arbitrarily defined. This allows for sparse and dense downsampled point clouds to be produced. The resolution may be determined by the user, or by the mapping manager based on, e.g., available computing resources, user preferences, default values, or other application-specific information. For example, a lower resolution (e.g., larger voxel size) may be used to produce a sparse downsampled point cloud for visualization on a client device or a mobile device. Additionally, or alternatively, outliers may be removed statistically. For example, the distance from each point to its nearest neighbor may be determined and statistically analyzed. If the distance from a point to its nearest neighbor is greater than a threshold value (e.g., a standard deviation of the nearest neighbor distances in the point cloud), then that point may be removed from the point cloud. In some embodiments, the outlier removal technique may be selectable by the user or be automatically selected by the mapping manager. In some embodiments, outlier removal may be disabled.

[0063] As discussed, the point cloud data may be a three-dimensional representation of the target environment. This 3D representation can be divided into voxels (e.g., 3D pixels).

[0064] After statistical outlier removal, the resulting point cloud data can be provided to map generator 316. In some embodiments, the map generator 316 may include a dense map generator 318 and/or a sparse map generator 320. In such embodiments, dense map generator 318 can produce a high-density map from the point cloud data received before outlier removal, and sparse map generator 320 can produce a low-density map from the sparse downsampled point cloud data received after outlier removal. In other embodiments, dense map generator 318 and sparse map generator 320 may produce a high-density map and a low-density map separately from the point cloud received both after outlier removal. In such embodiments, each map generator may generate the output map using the same process but may vary the size of the voxels to produce high-density or low-density maps. In some embodiments, the low-density map can be used by a client device or a mobile device to provide real-time visualization of the mapping data. The high-density map can be output as a LIDAR Data Exchange File (LAS) or other file type to be used with various mapping, planning, analysis, or other tools.

[0065] The map generator may use the point cloud data to perform a probabilistic estimation of the position of points in the map. For example, the map generator may use a 3D mapping library, such as OctoMap to produce the output map. The map generator can divide the point cloud data into voxels. For each voxel, the map generator can determine how many points are in the voxel and, based on the number of points and the variance associated with each point, determine the probability that a point is in that voxel. The probability may be compared to an occupancy threshold and, if the probability is greater than the occupancy threshold, a point may be represented in that voxel in the output map. In some embodiments, the probability that a given voxel is occupied can be represented as:

P .function. ( n .times. | .times. z 1 : t ) = [ 1 + 1 - P .function. ( n .times. | .times. z t ) P .function. ( n .times. | .times. z t ) .times. 1 - P ( n .times. | .times. z 1 .times. : .times. t - 1 ) P .function. ( n .times. | .times. z 1 : t - 1 ) .times. P .function. ( n ) 1 - P .function. ( n ) ] - 1 ##EQU00001##

[0066] The probability P(n|z.sub.1:t) of a node n being occupied is a function of the current measurement z.sub.1, a prior probability P(n), and the previous estimate P(n|z.sub.1:t-1). Additionally, P(n|z.sub.t) represents the probability that voxel n is occupied given the measurement z.sub.t. This probability may be augmented to include the variance of each point, as measured by the positioning sensor, as represented by the following equations:

P .function. ( n ) = 1 2 .times. P x .function. ( x , .mu. x , .sigma. x 2 ) .times. P y .function. ( y , .mu. y , .sigma. y 2 ) .times. P z .function. ( z , .mu. z , .sigma. z 2 ) + 1 2 ##EQU00002## P .function. ( n , .mu. , .sigma. 2 ) = 1 2 .times. .pi. .times. .sigma. 2 .times. e - ( x - .mu. ) 2 2 .times. .sigma. 2 ##EQU00002.2##

[0067] In the equations above, P(n) represents the total probability that a voxel n is occupied. The use of 1/2 in the above equation is implementation specific, such that the probability is mapped to a range of 1/2-1. This range may vary, depending on the particular implementation in use. In the above equations, the total probability is the product of probabilities calculated for the x, y, and z dimensions. The probability in each dimension may be determined based on the mean, .mu., for each point in that dimension, and the variance, .sigma..sup.2, of each measurement in a given dimension, with x, y, and z corresponding to the coordinate values of a given point. A large number of points near the mean point in a given voxel may increase the probability, while a more diffuse collection of points in the voxel may lower the probability. Likewise, a large variance associated with the data (e.g., indicating lower accuracy position data has been collected) may lower the probability while a lower variance may increase the probability. P(n, .mu., .sigma..sup.2) represents the Gaussian distribution for the voxel, given the mean and variance values of the points in that voxel.

[0068] If the total probability of a voxel being occupied is greater than a threshold occupancy value, then a point can be added to that voxel. In some embodiments, all of the points in that voxel can be averaged, and the resulting mean coordinate can be used as the location of the point in that voxel. This improves the accuracy of the resulting map over alternative methods, such as using the center point of an occupied voxel as the point, which may result in skewed results depending on the resolution of the voxels. In various embodiments, the occupancy threshold can be set based on the amount of processing resources available and/or based on the acceptable amount of noise in the data for a given application. For example, the occupancy threshold can be set to a default value of 70%. A higher threshold can be set to reduce noise. Additionally, the occupancy threshold may be set depending on the quality of the data being collected. For example, data collected under one set of conditions may be high quality (e.g., low variance) and a lower occupancy threshold can be set, while lower quality data may necessitate a higher occupancy threshold.

[0069] The resulting map data, with one point in each occupied voxel, can then be output as an LAS file, or other file format. In some embodiments, the geo-referenced point cloud data may be output without additional processing (e.g., outlier removal). In some embodiments, each point in the point cloud data may also be associated with an intensity value. The intensity value may represent various features of the object being scanned, such as elevation above a reference plane, material composition, etc. The intensity value for each point in the output map may be an average of the intensity values measured for each point in the mapping data collected by the scanning sensor (e.g., a LiDAR sensor).

[0070] FIGS. 4A and 4B illustrate an example of a hierarchical data structure, in accordance with various embodiments. As discussed above, and as shown in FIG. 4A, data representing a 3D environment 400 can be divided into a plurality of voxels. As shown in FIG. 4A, the target environment can be divided into eight voxels, with each voxel being further divided into eight sub-voxels, and each sub-voxel divided into eight further smaller sub-voxels. Each voxel may represent a different volumetric portion of the 3D environment. The voxels may be subdivided until a smallest voxel size is reached. The resulting 3D environment can be represented as a hierarchical data structure 402, where the root of the data structure represents the entire 3D environment, and each child node represents a different voxel in different hierarchy within the 3D environment.

[0071] FIGS. 5A and 5B illustrate an example of outlier removal in mapping data, in accordance with various embodiments. As shown in FIG. 5A, when a target object is scanned, it may be represented as a plurality of points, with those points clustered on different parts of the object, including surfaces (such as surface 501), edges (such as edge 503), and other portions of the target object in the target environment. For simplicity of depiction, these surfaces, edges, etc. are shown solid. In various regions 500A-500F of the data, there are additional outlier points. This may be most noticeable in regions of empty space, as shown in FIG. 5A. These points are diffuse, as compared to the more densely packed points of the surfaces and edges of the target object. Outlier removal may be used to eliminate or reduce the number of these points in the data. As discussed above, the geo-referenced point cloud data may be downsampled, reducing the number of outliers in the data. Additionally, or alternatively, outliers may be removed statistically. For example, the distance from each point to its nearest neighbor may be determined and statistically analyzed. If the distance from a point to its nearest neighbor is greater than a threshold value (e.g., a standard deviation of the nearest neighbor distances in the point cloud), then that point may be removed from the point cloud. As shown in FIG. 5B, following outlier removal, the regions of the point cloud data 502A-502F have been reduced, providing a cleaner 3D map.

[0072] FIG. 6 illustrates an example 600 of intensity values in mapping data, in accordance with various embodiments. As shown in FIG. 6, one example of intensity values may be to represent elevation above a reference plane. In this example, different elevation ranges may be assigned a different intensity value 602-606, as depicted here using greyscale coloration. In various embodiments, intensity may be represented using different colors to represent different values or ranges of values. Additionally, intensity may be used to represent different materials being scanned. For example, steel and concrete will absorb and reflect the incident radiation produced by the scanning sensor differently, enabling the scanning sensor to identify different materials in use. Each material may be encoded as a different intensity value associated with each point and represented by a different color in the output map. Additionally, although the example shown in FIG. 6 shows three greyscale colors representing different elevation ranges, in various embodiments, continuous gradients of colors may be used to represent continuous changes in elevation value above a reference plane.

[0073] FIG. 7 illustrates an example of supporting a movable object interface in a software development environment, in accordance with various embodiments. As shown in FIG. 7, a movable object interface 703 can be used for providing access to a movable object 701 in a software development environment 700, such as a software development kit (SDK) environment. In some embodiments, the movable object interface 703, may render a real-time map generated by the mapping manager and other interfacing components for receiving user input. The real-time map may be rendered on a display of a client device or other computing device in communication with the movable object. As used herein, the SDK can be an onboard SDK implemented on an onboard environment that is coupled to the movable object 701. The SDK can also be a mobile SDK implemented on an off-board environment that is coupled to a client device or a mobile device. As discussed above, the mapping manager can be implemented using an onboard SDK coupled to the movable object 701 or a mobile SDK coupled to a client device or a mobile device to enable applications to perform real-time mapping, as described herein.

[0074] Furthermore, the movable object 701 can include various functional modules A-C 711-713, and the movable object interface 703 can include different interfacing components A-C 731-733. Each said interfacing component A-C 731-733 in the movable object interface 703 corresponds to a module A-C 711-713 in the movable object 701. In some embodiments, the interfacing components may be rendered on a user interface of a display of a client device or other computing device in communication with the movable object. In such an example, the interfacing components, as rendered, may include selectable command buttons for receiving user input/instructions to control corresponding functional modules of the movable object.

[0075] In accordance with various embodiments, the movable object interface 703 can provide one or more callback functions for supporting a distributed computing model between the application and movable object 701.

[0076] The callback functions can be used by an application for confirming whether the movable object 701 has received the commands. Also, the callback functions can be used by an application for receiving the execution results. Thus, the application and the movable object 701 can interact even though they are separated in space and in logic.

[0077] As shown in FIG. 7, the interfacing components A-C 731-733 can be associated with the listeners A-C 741-743. A listener A-C 741-743 can inform an interfacing component A-C 731-733 to use a corresponding callback function to receive information from the related module(s).

[0078] Additionally, a data manager 702, which prepares data 720 for the movable object interface 703, can decouple and package the related functionalities of the movable object 701. The data manager 702 may be onboard, that is coupled to or located on the movable object 701, which prepares the data 720 to be communicated to the movable object interface 703 via communication between the movable object 701 and a client device or a mobile device. The data manager 702 may be off board, that is coupled to or located on a client device or a mobile device, which prepares data 720 for the movable object interface 703 via communication within the client device or the mobile device. Also, the data manager 702 can be used for managing the data exchange between the applications and the movable object 701. Thus, the application developer does not need to be involved in the complex data exchanging process. In some embodiments, mapping manager 126 may be one implementation of data manager 702. In such an embodiment, the mapping manager is used for managing mapping data, including generating a map using mapping data and positioning data and rendering the generated map for display based on a default setting or a user selection.

[0079] For example, the onboard or mobile SDK can provide a series of callback functions for communicating instant messages and for receiving the execution results from a movable object. The onboard or mobile SDK can configure the life cycle for the callback functions in order to make sure that the information interchange is stable and completed. For example, the onboard or mobile SDK can establish connection between a movable object and an application on a smart phone (e.g. using an Android system or an iOS system). Following the life cycle of a smart phone system, the callback functions, such as the ones receiving information from the movable object, can take advantage of the patterns in the smart phone system and update the statements accordingly to the different stages in the life cycle of the smart phone system.

[0080] FIG. 8 illustrates an example of a movable object interface, in accordance with various embodiments. As shown in FIG. 8, a movable object interface 803 can be rendered on a display of a client device or other computing devices representing statuses of different components of a movable object 801. Thus, the applications, e.g., APPs 804-806, in the movable object environment 800 can access and control the movable object 801 via the movable object interface 803. As discussed, these apps may include an inspection app 804, a viewing app 805, and a calibration app 806.

[0081] For example, the movable object 801 can include various modules, such as a camera 811, a battery 812, a gimbal 813, and a flight controller 814.

[0082] Correspondently, the movable object interface 803 can include a camera component 821, a battery component 822, a gimbal component 823, and a flight controller component 824 to be rendered on a computing device or other computing devices to receive user input/instructions by way of using the APPs 804-806.

[0083] Additionally, the movable object interface 803 can include a ground station component 826, which is associated with the flight controller component 824. The ground station component operates to perform one or more flight control operations, which may require a high-level privilege.

[0084] FIG. 9 illustrates an example of components for a movable object in a software development kit (SDK), in accordance with various embodiments. The SDK 900 may be an onboard SDK implemented on an onboard mapping manager or a mobile SDK implemented on mapping manager located on a client device or a mobile device. The SDK 900 may correspond to all or a portion of the mapping manager described above or may be used to implement the mapping manager as a standalone application. As shown in FIG. 9, the drone class 901 in the SDK 900 is an aggregation of other components 902-907 for a movable object (e.g., a drone). The drone class 901, which have access to the other components 902-907, can exchange information with the other components 902-907 and controls the other components 902-907.

[0085] In accordance with various embodiments, an application may be accessible to only one instance of the drone class 901. Alternatively, multiple instances of the drone class 901 can present in an application.

[0086] In the SDK, an application can connect to the instance of the drone class 901 in order to upload the controlling commands to the movable object. For example, the SDK may include a function for establishing the connection to the movable object. Also, the SDK can disconnect the connection to the movable object using an end connection function. After connecting to the movable object, the developer can have access to the other classes (e.g. the camera class 902, the battery class 903, the gimbal class 904, and the flight controller class 905). Then, the drone class 901 can be used for invoking the specific functions, e.g. providing access data which can be used by the flight controller to control the behavior, and/or limit the movement, of the movable object.

[0087] In accordance with various embodiments, an application can use a battery class 903 for controlling the power source of a movable object. Also, the application can use the battery class 903 for planning and testing the schedule for various flight tasks. As battery is one of the most restricted elements in a movable object, the application may seriously consider the status of battery not only for the safety of the movable object but also for making sure that the movable object can finish the designated tasks. For example, the battery class 903 can be configured such that if the battery level is low, the movable object can terminate the tasks and go home outright. For example, if the movable object is determined to have a battery level that is below a threshold level, the battery class may cause the movable object to enter a power savings mode. In power savings mode, the battery class may shut off, or reduce, power available to various components that are not integral to safely returning the movable object to its home. For example, cameras that are not used for navigation and other accessories may lose power, to increase the amount of power available to the flight controller, motors, navigation system, and any other systems needed to return the movable object home, make a safe landing, etc.

[0088] Using the SDK, the application can obtain the current status and information of the battery by invoking a function to request information from in the Drone Battery Class. In some embodiments, the SDK can include a function for controlling the frequency of such feedback.

[0089] In accordance with various embodiments, an application can use a camera class 902 for defining various operations on the camera in a movable object, such as an unmanned aircraft. For example, in SDK, the Camera Class includes functions for receiving media data in SD card, getting & setting photo parameters, taking photo and recording videos.

[0090] An application can use the camera class 902 for modifying the setting of photos and records. For example, the SDK may include a function that enables the developer to adjust the size of photos taken. Also, an application can use a media class for maintaining the photos and records.

[0091] In accordance with various embodiments, an application can use a gimbal class 904 for controlling the view of the movable object. For example, the Gimbal Class can be used for configuring an actual view, e.g. setting a first personal view of the movable object. Also, the Gimbal Class can be used for automatically stabilizing the gimbal, in order to be focused on one direction. Also, the application can use the Gimbal Class to change the angle of view for detecting different objects.

[0092] In accordance with various embodiments, an application can use a flight controller class 905 for providing various flight control information and status about the movable object. As discussed, the flight controller class can include functions for receiving and/or requesting access data to be used to control the movement of the movable object across various regions in a movable object environment.

[0093] Using the Flight Controller Class, an application can monitor the flight status, e.g. using instant messages. For example, the callback function in the Flight Controller Class can send back the instant message every one thousand milliseconds (1000 ms).

[0094] Furthermore, the Flight Controller Class allows a user of the application to investigate the instant message received from the movable object. For example, the pilots can analyze the data for each flight in order to further improve their flying skills.

[0095] In accordance with various embodiments, an application can use a ground station class 907 to perform a series of operations for controlling the movable object.

[0096] For example, the SDK may require applications to have an SDK-LEVEL-2 key for using the Ground Station Class. The Ground Station Class can provide one-key-fly, on-key-go-home, manually controlling the drone by app (i.e. joystick mode), setting up a cruise and/or waypoints, and various other task scheduling functionalities.

[0097] In accordance with various embodiments, an application can use a communication component for establishing the network connection between the application and the movable object.

[0098] FIG. 10 shows a flowchart of a method of target mapping in a movable object environment, in accordance with various embodiments. At operation/step 1002, mapping data can be obtained from a scanning sensor (e.g., a LiDAR sensor) supported by a movable object (e.g., a UAV). In some embodiments, the scanning sensor can be a LiDAR sensor. At operation/step 1004, positioning data can be obtained from a positioning sensor (e.g., a GPS sensor, an RTK sensor, an IMU sensor, and/or other positioning sensors or a combination thereof) supported by the movable object (e.g., a UAV). In some embodiments, the positioning sensor can be an RTK sensor or an IMU sensor.

[0099] At operation/step 1006, the mapping data can be associated with the positioning data based at least on time data associated with the mapping data and the positioning data. In some embodiments, associating the mapping data with the positioning data may include upsampling the positioning data to include a number of positions equal to a number of points in the mapping data, and associating each point in the mapping data with a corresponding position in the upsampled positioning data. In some embodiments, the time data associated with the mapping data and the positioning data may be obtained using clock circuitry providing a reference clock signal electronically coupled to the scanning sensor and the positioning sensor.

[0100] At operation/step 1008, a map in a first coordinate system may be generated based at least on the associated mapping data and positioning data. In some embodiments, generating the map may include, for each voxel of a plurality of voxels of the map, determining one or more points from the mapping data to be located in the voxel, and determining an occupancy probability for the voxel based at least on a number of points in that voxel. In some embodiments, the occupancy probability is determined based on a variance of the positioning data associated with the one or more points located in the voxel. In some embodiments, for each voxel having an occupancy probability greater than an occupancy probability threshold value, an average position of the one or more points in the voxel can be calculated, and a point can be generated in the map at the average position. In some embodiments, for each voxel having an occupancy probability greater than the occupancy probability threshold value, an average intensity value of the one or more points in the voxel can be calculated, and the average intensity value can be associated with the generated point in the map. In an embodiment, the average intensity value is calculated based on feature of each point in the voxel, where the feature of each point is associated with an elevation or a material detected by the scanning sensor.

[0101] In some embodiments, the method may further include determining a distribution of points in the mapping data, each of the points in the mapping data associated with a distance from a nearest neighboring point in the mapping data, and removing any points associated with a distance greater than a distance threshold value. In some embodiments, the method may further include downsampling the mapping data by a scaling factor, dividing the mapping data into a plurality of voxels, and outputting an average point from the downsampled mapping data for each of the plurality of voxels. In some embodiments, the method may further include transforming the map into a second coordinate system and outputting the transformed map. For example, the positioning data may be converted from the scanner reference frame to a north-east-down (NED) reference frame (or a NED coordinate system). The reference frame to which the positioning data is converted may vary depending on the application of the map that is being produced. For example, if the map is being used in surveying, it may be converted to the NED reference frame. For another example, if the map is being used for rendering motions such as flight simulation, it may be converted to the FlightGear coordinate system. Other applications of the map may effect conversions of the positioning data to different reference frames or different coordinate systems.

[0102] In some embodiments, geo-referencing as described above may be combined with scan matching, such as Simultaneous Localization and Mapping (SLAM) or LiDAR Odometry and Mapping (LOAM). Traditional methods make use of SLAM with or without inertial navigation input. For example, some methods inject IMU information with SLAM and sometimes inject odometry via GPS which provides an improved mapping algorithm. Unlike traditional methods, embodiments can perform direct geo-referencing as discussed above, and then a layer of SLAM or LOAM can be added on top of the geo-references. This provides a robust mapping algorithm as the geo-references serves as a floor on the quality of the resulting map.

[0103] In some embodiments, geo-referencing as described above may be combined with normal distribution transformation (NDT). NDT is a LiDAR scan registration method which is in between a feature-based registration method (such as LOAM) and a point-based registration method (such as iterative closest point). The "features" of the world are described by multivariate Gaussian distributions defined in each voxel. A probability density function (PDF) is generated for each cell and points are matched to the map by maximizing the sum of probability generated by the PDF, points x, and a transformation T:

T = arg .times. .times. min T .times. i = 1 k .times. - p i .function. ( Tx i ) ##EQU00003## p i .function. ( x i ) .about. N ( .mu. , .SIGMA. i ) .times. .mu. i = [ .mu. x .mu. y .mu. z ] ##EQU00003.2##

[0104] As discussed, in various embodiments, a movable object may be used for performing real-time mapping of various application environments, such as construction site mapping, surveying, target object mapping, etc. In some embodiments, the movable object may be an unmanned aerial vehicle (UAV), such as shown in FIG. 11, which has been configured to perform real-time mapping. FIG. 11 shows an isometric view 1100 of a movable object for performing real-time mapping, in accordance with an embodiment. As discussed above, a UAV in various embodiments may include a main body 1110. The main body may include, or be coupled to, a sensing system, a communications system, movement mechanisms, such as motors 1112 which may independently power rotors (not shown) to cause the UAV to fly and navigate a predefined route and/or a route based on real time user commands, and other systems and functional modules as discussed above.

[0105] As shown in FIG. 11, a UAV configured to perform real-time mapping may include a payload assembly (or a sensor assembly) 1102, which may include a scanning sensor and a positioning sensor (as discussed above), and a mounting assembly 1104 to connect the payload assembly to the movable object body. In some embodiments, the UAV may further include a landing gear assembly 1106 designed to provide a secure platform when not in flight and during landing/takeoff, while not interfering with the field of view (FOV) of the scanning sensor of payload assembly 1102. In some embodiments, the angle 1108 of the landing gear may be based on the FOV of the scanning sensor in use. This may include fixed landing gear, such as shown in FIG. 11, and adjustable landing gear, which may change the angle 1108 of the landing gear dynamically, based on the sensor in use.

[0106] FIG. 12 shows a rear view 1200 of a movable object (e.g., a UAV) for performing real-time mapping, in accordance with an embodiment. As shown in FIG. 12, a main body 1202 can be coupled to the mounting assembly 1104. In some embodiments, the mounting assembly can include expansion brackets 1204 which are coupled to the main body 1202 using one or more fasteners, and which provide clearance for various components of the movable object, such as batteries, onboard computing device 1206, and other components. The mounting assembly may further include a base plate 1208 coupled to the expansion brackets using a plurality of dampers 1210. In some embodiments, the payload assembly 1102 including a LiDAR/global navigation satellite service (GNSS) IMU system is secured to the underside of the movable object via the mounting assembly using a plurality of mounting points of the base plate 1208. Vibration isolation is provided to the LiDAR/GNSS IMU system via the base plate 1208 resting on the plurality of dampers 1210.

[0107] As shown in FIG. 12, base plate 1208 may include dovetail mounts 1212. In various embodiments, the dovetail mounts 1212 enable the user to slide the payload assembly 1102 (e.g., including a LiDAR/GNSS IMU system) in position and secure with two fasteners, such as M4 wingnuts or other suitable fasteners. This enables the payload assembly, including the LiDAR/GNSS IMU system to be easily removed from the movable object via the mounting assembly. In some embodiments, the angle 1216 of the landing gear legs from the movable object may be adjustable, depending on the size of the payload, batteries, or other components and/or based on the FOV of the scanning sensor or other sensors included in the payload.

[0108] FIG. 13 shows an isometric exploded view 1300 of the mounting assembly and payload assembly, in accordance with an embodiment. As shown in FIG. 13, mounting assembly 1104 may include base plate 1208 which is coupled to the expansion brackets 1204 at a plurality of locations 1304. For example, as shown in FIG. 13, the lower end of each expansion bracket (e.g., the end closest to the payload assembly) may include a hole which aligns with a corresponding hole on the base plate 1208. Each location may include a damper that, when assembled, is under compression between the base plate 1208 and the expansion brackets 1204. Each damper may be made of a compressible material, such as a natural or synthetic rubber, thermoplastic elastomer, or other shock absorbing material. The dampers may be secured between the base plate 1208 and the expansion brackets 1204 at the plurality of locations. For example, each damper may include flared ends. A lower flared end may be forced through a hole in an expansion bracket 1204 and an upper flared end may be forced through a hole in the base plate 1208. Such an arrangement couples the base plate 1208 to the expansion brackets 1204 using the plurality of dampers. In the example shown in FIG. 13, there may be six dampers coupling the base plate 1208 to the expansion brackets 1204, three on either side of the base plate 1208. However, the base plate 1208 may be coupled to the expansion brackets 1204 at more or fewer locations, in accordance with various embodiments.

[0109] The base plate 1208 may further include a plurality of holes 1306 which line up with holes 1308 of the payload assembly when assembled via the dovetails. A fastener may be inserted through the aligned holes to secure the payload assembly to the base plate 1208. As shown in FIG. 13, the payload assembly may include two payload support brackets 1302. Each payload support bracket may include a dovetail which enables the payload support bracket to be connected to the dovetail groove in the base plate 1208. Alternatively, in some embodiments, the base plate 1208 may include a dovetail that can be inserted into a dovetail groove in each payload support bracket 1302. The payload assembly may further include a pivot bracket 1312. The pivot bracket can be connected to scanning sensor 1310 (such as a LiDAR sensor) using one or more fasteners. The pivot bracket may include one or more pivot arms 1314 which can be connected to the payload support brackets 1302. For example, in the embodiment of FIG. 13, the pivot bracket includes two pivot arms 1314. A hole 1316 in each pivot arm can be aligned with a hole 1318 in each payload support bracket 1302 to secure the scanning sensor 1310 at a particular scanning angle. In various embodiments, the payload support bracket can be secured to the pivot bracket using any suitable fastener which is removable such that the pivot bracket can be pivoted to another scanning angle (e.g., aligned with a different hole in the payload support bracket) and then recoupled to change the scanning angle of the scanning sensor 1310.

[0110] As shown in FIG. 13, the dovetail design on the pivot bracket enables the LiDAR/GNSS IMU system to be quickly removed. The pivot bracket 1312 may further include at least one mounting point 1319 to which a positioning sensor 1320 (e.g., a GNSS IMU system, an RTK system, an RTK/IMU system, etc.) can be attached. By mounting the pivot bracket 1312 to the scanning sensor 1310 on one side of the pivot bracket 1312 and the positioning sensor 1320 on the other side of the pivot bracket 1312, any relative motion between the two sensors is eliminated or greatly reduced. The positioning sensor 1320 can be bolted, screwed, epoxied, or be otherwise fixedly coupled to the pivot bracket 1312. In some embodiments, the positioning sensor 1320 may be permanently coupled to the pivot bracket 1312 or may be removably coupled to the pivot bracket 1312. The positioning sensor 1320 may be protected from the elements and/or electromagnetic interference using a positioning sensor enclosure 1322 which may be coupled to the pivot bracket 1312. The positioning sensor enclosure 1322 provides ingress protection (IP) for the electronics from foreign debris and moisture. In some embodiments, the enclosure 1322 is sprayed with a thin layer of paint or other substance to protect the GNSS IMU from jamming caused by electromagnetic interference. This may include copper paint, or other material suitable to preventing jamming due to electromagnetic interference.

[0111] Additionally, in some embodiments, an onboard computing device 1206 (such as computing device 112 described above) may be coupled to the base plate 1208 using a computing device bracket 1324. In some embodiments, expansion brackets 1204 can be stabilized using alignment brackets 1326. These can ensure that the expansion brackets 1204 remain parallel while in flight and eliminate or reduce undesirable twisting of the mounting assembly which might affect the reliability of the sensor data, such as mapping data and positioning data, collected by the scanning sensor and positioning sensor.

[0112] FIG. 14 shows an isometric view 1400 of base plate 1208, in accordance with some embodiments. Base plate 1208 can include the plurality of mounting locations 1402 at which the dampers may be used to couple the base plate to the expansion brackets, as discussed above. Additionally, mounting holes 1306 may be located above the dovetail grooves 1404, with the holes penetrating from the surface of the base plate 1208 to the dovetail grooves 1404, allowing them to be aligned with holes of the payload support interface as discussed above.

[0113] FIG. 15 shows an isometric assembled view 1500 of the mounting assembly and payload assembly, in accordance with an embodiment. As shown in FIG. 15, the dovetails of payload support brackets 1302 are inserted into the dovetail grooves of base plate 1208. Positioning sensor enclosure 1322 is in place covering the positioning sensor and coupled to the pivot bracket. In the embodiment of FIG. 15, the pivot arms are aligned with an intermediate hole of the payload support brackets 1302, causing the scanning sensor to be set at an angle between 90 degrees and 0 degrees, such as 35 degrees relative to the base plate 1208 or a horizontal plane when a UAV (e.g., as shown above with respect to FIG. 11) is in its landing pose. The expansion brackets 1204 and alignment brackets 1326 can be coupled to a UAV (e.g., as shown above with respect to FIG. 11), to secure the mounting assembly to the UAV for mapping missions, as discussed above.

[0114] FIGS. 16A-16D show additional views 1600-1606 of the payload assembly in accordance with various embodiments. As shown in FIG. 16A at 1600, the pivot bracket 1312 may include a plurality of mounting points 1608 to which the positioning sensor may be coupled. As shown in FIG. 16B at 1602, the positioning sensor can be mounted to the plurality of mounting points 1608 by aligning a plurality of mounting holes 1610 in the positioning sensor 1320 and securing the positioning sensor 1320 to the mounting points 1608 using fasteners, such as screws or other suitable fasteners. As shown in FIG. 16C, at 1604, the payload support brackets 1302 can be coupled to the pivot brackets at pivot arms 1314. As discussed, the pivot arms can be aligned to corresponding holes on the payload support brackets to secure the scanning sensor 1310 at a predefined scanning angle. In some embodiments, the payload support brackets 1302 may include grooves to which the pivot arms 1304 may be coupled, enabling a selection of a range of angles rather than particular angles predefined by the hole placements in the payload support brackets. As shown in FIG. 16D, at 1606, the positioning sensor enclosure 1322 can be secured to the pivot bracket to protect the positioning sensor from debris, electromagnetic interference, and/or other environmental hazards. As discussed, the assembled payload assembly may be connected to the base plate of the mounting assembly using dovetails and coupled to the base plate by aligning holes 1308 with corresponding holes in the base plate and securing with a suitable fastener.

[0115] FIG. 17 shows an alternative enclosure 1700 to prevent jamming of the positioning sensor of a movable object in accordance with various embodiments. In order to prevent the GNSS-IMU from jamming due to electromagnetic inference, an aluminum enclosure can be added which serves as a Faraday cage with its various circular cutouts. The size and locations of the circular cutouts may be selected for the frequency or frequencies of electromagnetic interference that are expected and/or those frequencies most likely to interfere with the functioning of the IMU.

[0116] FIGS. 18A and 18B show example alignments of lower expansion brackets in accordance with various embodiments. As shown at 1800 and 1802, an alignment bracket 1326 can provide alignment of the expansion brackets such that the expansion brackets remain in parallel to one another. Absent the alignment brackets, the expansion brackets may freely rotate in place after installation on the movable object. Thus, there is a need to constrain the expansion brackets such that the back planes of the brackets remain parallel. In some embodiments, the alignment bracket may include a square (or other shaped) extension 1804. This may be inserted into correspondingly shaped holes 1806 in the expansion brackets 1204.

[0117] FIG. 19 shows an example 1900 of the alignment bracket 1326 being connected to the movable object body 1202 and the expansion brackets 1204, in accordance with an embodiment. In some embodiments, two threaded screw holes can be used: a first for alignment and a second for mounting on the movable object. For example, movable object body 1202 may include holes 1902 through which a screw may be inserted and screwed into a first threaded screw hole of alignment bracket 1326. Alignment bracket 1326 may further include a second threaded screw hole 1904 which may be aligned with a hole 1906 in expansion brackets 1204, as shown in FIG. 19.

[0118] FIG. 20 shows an alternative 2000 mechanical attachment of the payload assembly (including a scanning sensor and a positioning sensor, as discussed above) to a movable object via a mounting assembly, in accordance with various embodiments. Plate 2002 is fastened to the underside of the movable object directly or indirectly via the mounting assembly, and plate 2004 can be fastened to the payload assembly. The two plates can be coupled using a plurality of dampers 2006 which are under compression when assembled. A fastener (such as a wingnut or other suitable fastener) can be attached into the bottom of the rod piece 2008 inserted through plates 2002 and 2004 and fastened to the payload assembly through the hole 2010 in a crossbar 2012 connecting the payload support brackets 1302, making the payload assembly easily removable. In some embodiments, plate 2002 may be coupled to the base plate of the mounting assembly described above or may be used to replace the base plate of the mounting assembly. In other embodiments, plate 2002 may be coupled directly to the main body of a movable object (e.g., an UAV).

[0119] In some embodiments, a mirror or a plate with a reflective coating material may be installed on the scanning sensor (such as the LiDAR sensor) via the fastener, at a certain angle that overlaps with at least a portion of the FOV of the scanning sensor in use. By way of applying the mirror or the plate with the reflective coating material, the FOV of the scanning sensor may be broadened to include a second FOV that is created by laser lights illuminated from the scanning sensor that are being reflected by the mirror or the plate with the reflective coating material.

[0120] FIGS. 21-23 show an alternative mechanical attachment of the LiDAR and positioning sensor to a movable object in accordance with various embodiments. As shown in FIG. 21, the alternative mechanical attachment shown at 2100 may include a payload assembly similar to that discussed above. The payload assembly may include payload support brackets 2102 coupled by a crossbar 2104. A T-extrusion member 2106 can be fastened to an upper surface of the crossbar (e.g., the surface closest to the movable object). The T-extrusion member may be permanently coupled to the crossbar (e.g., welded, epoxied, or otherwise fixedly coupled) or fastened using one or more removable fasteners. A long axis 2108 of the T-extrusion member may be substantially orthogonal to a long axis 2110 of a clearance slot in alternative base plate 2112. FIG. 22 shows an alternative view 2200 of the mechanical attachment. To attach the payload assembly, the payload assembly can be rotated 90 degrees relative to the alternative base plate 2112 such that the long axis 2108 of the T-extrusion member is aligned with the long axis 2110 of the clearance slot and the T-extrusion member can be raised through the clearance slot. For example, as shown in FIG. 23 the T-extrusion member 2106 has been raised through the clearance slot of the alternative base plate 2112 and then the payload assembly has been rotated 90 degrees in the opposite direction. Once positioned as shown in FIG. 23, the T-extrusion member can be secured to the top pressure plate 2300 with fasteners (e.g., wingnuts or other suitable fasteners). The top pressure plate 2300 can be coupled to the alternative base plate 2112 using a plurality of dampers 2302 to reduce the movement of the payload assembly relative to the alternative base plate 2112.

[0121] FIG. 24 shows an example 2400 of a landing gear in accordance with various embodiments. As shown in FIG. 24, the landing gear legs 2402 may be angled 1108 based on the field of view (FOV) of the scanning sensor 1310. For example, in the embodiment of FIG. 24, the landing gear legs 2402 may be at a fixed angle of 55 degrees (e.g., measured in the plane formed by the landing gear legs) to accommodate the FOV of the particular scanning sensor in use. Additionally, or alternatively, the angle 1108 of the landing gear legs 2402 may be adjusted, manually or automatically, based on the FOV of the scanning sensor in use. In some embodiments, the landing gear legs 2402 may be coupled to the movable object using a landing gear bracket 2404. The landing gear bracket can provide the fixed angle 1108 of the landing gear legs 2402. The landing gear bracket can be connected to the movable object using connecting member 2406. In some embodiments, the connecting member 2406 and the landing gear legs 2402 can be made of the same material. In some embodiments, the connecting member can connect to a landing gear mounting bracket of the movable object body via a quick release connection.

[0122] FIG. 25 shows an example 2500 of a landing gear bracket 2404 in accordance with various embodiments. In some embodiments, the landing gear bracket 2404 can secure the landing gear legs 2402 as well as provide shock absorption for the landing gear legs. For example, to improve upon the landing gear performance from drops and other shocks, the landing gear bracket 2404 may include a rubber (such as, SPE I synthetic elastomer) damper to fill the void at the location where the landing gear legs and connection member (such as carbon fiber tubes) intersect. This rubber damper helps to absorb and dissipate energy during an impulse force.

[0123] FIG. 26 shows an example 2600 of an alternative landing gear mounting point in accordance with various embodiments. A mounting point 2602 can be used to attach landing gear legs on the movable object such that the landing gear remains outside the field of view of the scanning sensor. This design uses the space adjacent to the motor heat sinks 2604 to attach the landing gear to the movable object arms. Using this small area helps to improve the vertical alignment of landing legs. In some embodiments, a landing gear leg can be attached adjacent to each motor heat sink. For example, if the movable object is a quadcopter with four motors and corresponding heat sinks, then four landing gear mounting points can be provided with four landing gear legs. In some embodiments, at least three landing gear mounting points and associated landing gear legs may be provided regardless of the number of motors equipped on the movable object.

[0124] FIGS. 27-29 show LiDAR fields of view in accordance with various embodiments. In the example 2700 shown in FIG. 27, the LiDAR is positioned to scan at 35 degrees. The LiDAR's FOV is in between the two planes 2702. In this position the FOV of the LiDAR would intersect the traditional landing gear assembly 2704 (shown dashed to indicate where it would be located if it were provided). As shown, the traditional landing gear assembly 2704 would partially obstruct the FOV of the scanning sensor. As such, to obtain a complete scan of an area would require additional scanning missions to be performed that account for the blind spots introduced by the traditional landing gear assembly. To address this, the angled landing gear assembly 2706 can include angled legs, as discussed above. As discussed, the landing gear legs may be angled depending on the FOV of the scanning sensor in use. As shown in FIG. 27, when so angled, the landing gear legs remain outside of LiDAR's field of view at the 35.degree. position. This eliminates the obstructions caused by the traditional landing gear assembly, leading to more efficient scanning missions. FIGS. 28 and 29 show the LiDAR FOV at its 90.degree. position. In the example 2800 of FIG. 28, the UAV is shown from the side view, with the LiDAR positioned to scan at 90 degrees. The FOV 2802 of the LiDAR in this position is obstructed by the traditional landing gear assembly 2704, similar to that discussed above with respect to FIG. 27. However, the angled landing gear assembly 2706 does not obstruct the FOV 2802 of the LiDAR in this position. FIG. 29 shows an isometric view 2900 of the UAV with the LiDAR in the 90-degree position. As discussed with respect to FIG. 28, the angled landing gear assembly 2706 does not obstruct the FOV 2802 in this position as the traditional landing gear assembly 2704 would.

[0125] FIGS. 30-32 show examples of angled positions of a scanning sensor coupled to a movable object, in accordance with various embodiments. In the example 3000 shown in FIG. 30, the LiDAR 1310 can be positioned at 0 degrees relative to horizontal. As discussed above, this position can be achieved using the pivot bracket 1312 and the payload support brackets 1302. In the example 3100 shown in FIG. 31, the LiDAR 1310 can be positioned at 35 degrees relative to horizontal. This angle position may also be achieved using the payload support brackets 1302 and the pivot bracket 1312, by aligning corresponding holes in the brackets for the 35-degree position. Similarly, the example 3200 shown in FIG. 32 shows the LiDAR 1310 positioned at 90 degrees relative to horizontal. As discussed above, this position may be achieved by changing the alignment of holes in the pivot bracket 1312 to corresponding holes in the payload support bracket 1302. In some embodiments, rather than holes which provide predefined angular positions, the payload support brackets 1302 may include slots, which enable the user to select various angular positions.

Payload Support Bracket

[0126] FIG. 33 shows example 3300 scanning patterns that may be implemented by LiDAR sensors that may be used in various embodiments. A LiDAR system is an active sensing system that emits light beams and measures a two-way travel time (i.e. time-of-flight) for the reflected light detected by the LiDAR sensor. The collected sensor data may generally be used to measure a range or a distance to an object which has reflected the light emitted by the LiDAR. Further, the object's position in a three-dimensional space (e.g., recorded with x-, y-, and z-coordinates, or latitude, longitude, and elevation values, or other coordinate systems, etc.) may be determined using (1) the detected two-way travel time of the emitted light beam, (2) the scanning angle of the light beam in reference to the three-dimensional space, and/or (3) the absolute location of the LiDAR sensor detected using a GPS, GNSS, INS or IMU sensor, etc.

[0127] Different LiDAR sensors may be associated with different scan patterns, scan frequencies, and/or scan angles. The scan patterns of a LiDAR sensor can be virtually any waveform by way of utilizing different scanning mechanisms (e.g., using a constant-velocity rotating polygon mirror or an oscillating mirror). Some examples of scan patterns include parallel scan lines, which may be generated by a rotating polygon mirror, or sawtooth scan lines which may be generated by an oscillating mirror. Other examples may include a sinusoidal scan pattern 3302, sawtooth scan pattern 3304, elliptical scan pattern 3306, spiral scan pattern 3308, or flower shape scan pattern 3310, or uniform scan pattern 3312 (which may be a series of concentric scans, such as circular, oval, or other scan shapes).

[0128] LiDAR data may be collected or recorded as discrete points or as a full waveform. Discrete points identify and record points at each peak location in the waveform curve. A full waveform records a distribution of returned energy and thus captures more information compared to discrete points. Whether collected as discrete points or full waveform, LiDAR data are available as discrete points, which is known as a LiDAR point cloud. LiDAR point cloud is usually stored as .las format (or .laz format, which is a highly compressed version of .las). Each lidar point data and its metadata may include various data attributes, such as associated coordinate values, an intensity value representing the amount of light energy recorded by the sensor, or classification data representing the type of object the laser return reflected off of (such as classified as ground or non-ground, as different altitudes, or as different material features), etc.

[0129] Many features can be performed in, using, or with the assistance of hardware, software, firmware, or combinations thereof. Consequently, features may be implemented using a processing system (e.g., including one or more processors). Exemplary processors can include, without limitation, one or more general purpose microprocessors (for example, single or multi-core processors), application-specific integrated circuits, application-specific instruction-set processors, graphics processing units, physics processing units, digital signal processing units, coprocessors, network processing units, audio processing units, encryption processing units, and the like.

[0130] Features can be implemented in, using, or with the assistance of a computer program product which is a storage medium (media) or computer readable medium (media) having instructions stored thereon/in which can be used to program a processing system to perform any of the features presented herein. The storage medium can include, but is not limited to, any type of disk including floppy disks, optical discs, DVD, CD-ROMs, microdrive, and magneto-optical disks, ROMs, RAMs, EPROMs, EEPROMs, DRAMs, VRAMs, flash memory devices, magnetic or optical cards, nanosystems (including molecular memory ICs), or any type of media or device suitable for storing instructions and/or data.

[0131] Stored on any one of the machine readable medium (media), features can be incorporated in software and/or firmware for controlling the hardware of a processing system, and for enabling a processing system to interact with other mechanism utilizing the results. Such software or firmware may include, but is not limited to, application code, device drivers, operating systems and execution environments/containers.

[0132] Features of the invention may also be implemented in hardware using, for example, hardware components such as application specific integrated circuits (ASICs) and field-programmable gate array (FPGA) devices. Implementation of the hardware state machine so as to perform the functions described herein will be apparent to persons skilled in the relevant art.

[0133] Additionally, the present invention may be conveniently implemented using one or more conventional general purpose or specialized digital computer, computing device, machine, or microprocessor, including one or more processors, memory and/or computer readable storage media programmed according to the teachings of the present disclosure. Appropriate software coding can readily be prepared by skilled programmers based on the teachings of the present disclosure, as will be apparent to those skilled in the software art.

[0134] While various embodiments have been described above, it should be understood that they have been presented by way of example, and not limitation. It will be apparent to persons skilled in the relevant art that various changes in form and detail can be made therein without departing from the spirit and scope of the invention.

[0135] The present invention has been described above with the aid of functional building blocks illustrating the performance of specified functions and relationships thereof. The boundaries of these functional building blocks have often been arbitrarily defined herein for the convenience of the description. Alternate boundaries can be defined so long as the specified functions and relationships thereof are appropriately performed. Any such alternate boundaries are thus within the scope and spirit of the invention.

[0136] The foregoing description has been provided for the purposes of illustration and description. It is not intended to be exhaustive or to limit the invention to the precise forms disclosed. The breadth and scope should not be limited by any of the above-described exemplary embodiments. Many modifications and variations will be apparent to the practitioner skilled in the art. The modifications and variations include any relevant combination of the disclosed features. The embodiments were chosen and described in order to best explain the principles of the invention and its practical application, thereby enabling others skilled in the art to understand the invention for various embodiments and with various modifications that are suited to the particular use contemplated. It is intended that the scope of the invention be defined by the following claims and their equivalence.

[0137] In the various embodiments described above, unless specifically noted otherwise, disjunctive language such as the phrase "at least one of A, B, or C," is intended to be understood to mean either A, B, or C, or any combination thereof (e.g., A, B, and/or C). As such, disjunctive language is not intended to, nor should it be understood to, imply that a given embodiment requires at least one of A, at least one of B, or at least one of C to each be present.

Claims

1. An unmanned aerial vehicle (UAV), comprising: a propulsion system; a main body coupled to the propulsion system; and a payload assembly coupled to the main body via a mounting assembly, wherein the payload assembly includes a payload comprising a scanning sensor and a positioning sensor, the payload assembly configured to orient the scanning sensor at a plurality of angles relative to the main body.

2. The UAV of claim 1, wherein the payload assembly comprises a plurality of payload support brackets configured to couple the payload assembly to the mounting assembly, the plurality of payload support brackets configured to provide the plurality of angles relative to the main body at which the payload can be oriented.

3. The UAV of claim 2, wherein the payload assembly comprises a pivot bracket configured to couple the scanning sensor and the positioning sensor, the pivot bracket configured to be aligned with the plurality of angles provided by the plurality of payload support brackets for changing a scanning angle of the scanning sensor.

4. The UAV of claim 3, wherein the scanning sensor is mounted to a side of the pivot bracket and the positioning sensor is mounted to another side of the pivot bracket.

5. The UAV of claim 1, wherein the plurality of angles includes angles corresponding at least to angles of 0 degrees, 35 degrees, or 90 degrees relative to the main body.

6. The UAV of claim 2, wherein the plurality of payload support brackets are connected to the mounting assembly using a dovetail quick release connection.

7. The UAV of claim 6, wherein the plurality of payload support brackets are connected to a base plate of the mounting assembly, the base plate having a plurality of dovetail grooves.

8. The UAV of claim 7, wherein the base plate is coupled to the mounting assembly using a plurality of dampers.

9. The UAV of claim 9, wherein the landing gear bracket include compressible materials configured to absorb or dissipate energy of an impulse force when landing.

10. The UAV of claim 9, wherein each landing gear assembly is coupled to the main body on an arm of the main body adjacent to a motor heat sink.

11. The UAV of claim 1, wherein the mounting assembly comprises a dampened plate assembly configured to couple the payload assembly to the main body, the dampened plate assembly comprising a first plate coupled to the main body and a second plate coupled to the first plate via a plurality of dampers, wherein a fastener is inserted through the dampened plate assembly and the payload assembly.

12. The UAV of claim 18, wherein a reflective member is coupled to the mounting assembly via the fastener, wherein the reflective member is positioned to overlap with at least a portion of a field of view (FOV) of the scanning sensor to cause the FOV of the scanning sensor to be broadened to include a second FOV comprising a reflection off of the reflective member.

13. The UAV of claim 19, wherein the reflective member includes a mirror or a plate including a reflective coating.

14. The UAV of claim 1, wherein the mounting assembly includes a plate assembly, the plate assembly comprising a first plate coupled to the main body via a plurality of expansion brackets and a second plate coupled to the first plate via a plurality of dampers, wherein a portion of the payload assembly is inserted through a portion of the first plate, and wherein the portion of the payload assembly is coupled to the second plate using a fastener.

15. The UAV of claim 21, wherein the plurality of expansion brackets includes at least two pairs of expansion brackets coupled to the main body, wherein each pair of expansion brackets are coupled to each other via an alignment bracket to maintain a parallel back plane of the pair of expansion brackets.

16. The UAV of claim 1, wherein the scanning sensor is a light detection and ranging (LiDAR) sensor.

17. The UAV of claim 23, wherein the LiDAR sensor implements a scanning pattern, the scanning pattern including at least one of a spiral pattern or a flower pattern.

18. The UAV of claim 1, wherein the scanning sensor is fixed at one of the plurality of angles during a scanning mission.

19. An unmanned aerial vehicle (UAV), comprising: a propulsion system; a main body coupled to the propulsion system; a payload assembly coupled to the main body via a mounting assembly, wherein the payload assembly includes a payload comprising a scanning sensor and a positioning sensor, the payload assembly configured to orient the scanning sensor at a plurality of angles relative to the main body; and at least two landing gear assemblies, each landing gear assembly including landing gear legs coupled to the main body using a landing gear bracket, wherein the landing gear bracket couples the landing gear legs at fixed angles to clear the landing gear legs from a field of view (FOV) of the scanning sensor.

20. An unmanned aerial vehicle (UAV), comprising: a propulsion system; a main body coupled to the propulsion system; and a payload assembly coupled to the main body via a mounting assembly, wherein the payload assembly includes a payload comprising a scanning sensor coupled to a positioning sensor via a pivot bracket, the payload assembly configured to orient the scanning sensor at a plurality of angles relative to the main body using the pivot bracket, and wherein the payload assembly comprises a positioning sensor enclosure covering the positioning sensor, the positioning sensor enclosure mounted to a side of the pivot bracket mounting the positioning sensor that is opposite to another side of the pivot bracket mounting the scanning sensor.