U.S. patent application number 14/588457 was filed with the patent office on 2015-06-04 for camera-style lidar system and method.
This patent application is currently assigned to Arete Associates. The applicant listed for this patent is Arete Associates. Invention is credited to Jeff T. Daiker, David M. Kane, James T. Murray.
Application Number | 20150153453 14/588457 |
Document ID | / |
Family ID | 42284556 |
Filed Date | 2015-06-04 |
United States Patent
Application |
20150153453 |
Kind Code |
A1 |
Kane; David M. ; et
al. |
June 4, 2015 |
CAMERA-STYLE LIDAR SYSTEM AND METHOD
Abstract
An apparatus aspect of the disclosure includes a lidar
transmitter emitting laser beams, and scan mirrors (or assemblies)
angularly adjustable to deflect the beams in orthogonal directions.
In one aspect, afocal optics magnify deflection, a transmitter
aperture transmits the beam, and a lidar receiver doesn't share the
transmitter aperture. In another aspect, auxiliary optics calibrate
the deflection. A method aspect of the disclosure includes noticing
and responding to a remote source, using a local laser, adjustable
scan mirror or assembly, afocal deflection magnifier, transmission
aperture and separate receiver. Method steps described include
operating the receiver to notice and determine the location of the
remote source, and controlling the transmitter to direct laser
light back toward that location.
Inventors: |
Kane; David M.; (Tucson,
AZ) ; Daiker; Jeff T.; (Tucson, AZ) ; Murray;
James T.; (Longmont, CO) |
|
Applicant: |
Name |
City |
State |
Country |
Type |
Arete Associates |
Northridge |
CA |
US |
|
|
Assignee: |
Arete Associates
Northridge
CA
|
Family ID: |
42284556 |
Appl. No.: |
14/588457 |
Filed: |
January 1, 2015 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
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12317771 |
Dec 29, 2008 |
8958057 |
|
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14588457 |
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PCT/US07/14992 |
Jun 26, 2007 |
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12317771 |
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60816656 |
Jun 27, 2006 |
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Current U.S.
Class: |
356/5.01 ;
356/4.01 |
Current CPC
Class: |
G01S 17/42 20130101;
G01S 7/481 20130101 |
International
Class: |
G01S 17/42 20060101
G01S017/42; G01S 7/481 20060101 G01S007/481 |
Goverment Interests
STATEMENT OF GOVERNMENT SUPPORT
[0002] This invention was made with government support under
contract W911 QX-04-C-0024 awarded by the Department of the Army.
The government has certain rights in the invention.
Claims
1. A method for noticing for and responding to a remote light
source, said method utilizing a transmitter which includes a local
radiation source that produces a laser beam, a scan mirror or
scan-mirror assembly angularly adjustable to deflect the beam in at
least two orthogonal directions, and an afocal optical unit for
magnifying the beam deflection, said transmitter having an aperture
for transmitting the beam; and a radiation receiver that does not
share the transmitter aperture, and an additional receiver, said
method comprising the steps of: operating the first-mentioned
receiver to notice and determine a location of the remote source;
controlling the transmitter to direct the laser beam back toward
the determined location; and activating the additional receiver to
collect and interpret reflected radiation of the back-directed
laser beam, received from the location; wherein the first-mentioned
receiver and the additional receiver are sensitive in respective
different wavelength bands, namely: a first spectral waveband
encompassing emissions of expected remote sources including but not
necessarily limited to said remote light source; and a second
spectral waveband encompassing said laser beam.
2. A method for noticing and responding to a remote light source,
said method utilizing a transmitter which includes a local
radiation source that produces a laser beam, a scan mirror or
scan-mirror assembly angularly adjustable to deflect the beam in at
least two orthogonal directions, and an afocal optical unit for
magnifying the beam deflection, said transmitter having an aperture
for transmitting the beam; and a radiation receiver that does not
share the transmitter aperture; further utilizing an additional
receiver, said method comprising the steps of: operating the
receiver to notice and determine a location of the remote source;
and controlling the transmitter to direct the laser beam back
toward the determined location; activating the additional receiver
to collect and interpret reflected radiation of the back-directed
laser beam, received from the location; wherein the activating step
comprises using the additional receiver in a lidar operating mode
to determine return time of the laser beam and thereby distance of
a reflecting object at the location.
3. A method for noticing and responding to a remote light source,
said method utilizing a transmitter which includes a local
radiation source that produces a laser beam, a scan mirror or
scan-mirror assembly angularly adjustable to deflect the laser beam
in at least two orthogonal directions, and an afocal optical unit
for magnifying the beam deflection, said transmitter having an
aperture for transmitting the beam; and a radiation receiver that
does not share the transmitter aperture; said method comprising the
steps of: operating the receiver to notice and determine a location
of the remote light source; and controlling the transmitter to
direct the laser beam back toward the determined location; wherein
the operating step comprises: fitting the centroid of an incoming
radiation pattern to an expected shape, when the laser-beam
divergence exceeds the per-pixel FOV.
Description
PRIORITY STATEMENT
[0001] This application is a continuation of U.S. application Ser.
No. 12/317,771, filed Dec. 29, 2008, which is a continuation of PCT
Application #PCT/US07/014,992, filed Jun. 26, 2007, which claims
priority to U.S. Provisional Application #60/816,656, filed Jun.
26, 2006.
BACKGROUND
[0003] The present system maintains the good pointing accuracy of
those earlier shared-aperture or shared-beam systems, but by a
different strategy as explained below. The aperture- or
beam-sharing systems suffer from an intrinsic limitation that the
light-transfer efficiency of the system for reception purposes is
constrained to be the same as for transmission purposes--whereas
the latter is held to the relatively small values appropriate for
MEMS beam steering.
[0004] Thus the prior art, and even our own earlier efforts to
provide uniformly excellent imaging quality with rapid operation,
continue to leave some further refinements to be desired.
SUMMARY OF THE DISCLOSURE
[0005] The present invention provides just such refinement. In
preferred embodiments the invention has several independent aspects
or facets, which are advantageously used in conjunction together
although they are capable of practice independently.
[0006] In its first main facet or aspect, the invention is lidar
apparatus. It includes a lidar transmitter having a laser source
that produces a laser beam, a scan mirror or scan-mirror assembly
angularly adjustable to deflect the beam in at least two orthogonal
directions, and an afocal optical unit for magnifying the beam
deflection.
[0007] In the apparatus, the transmitter has an aperture for
transmitting the beam. The apparatus also includes a lidar receiver
that does not share the transmitter aperture.
[0008] The foregoing may be a definition or description of the
first aspect of the invention in its broadest or most general form.
Even as thus broadly couched, however, it can be seen that this
facet of the invention significantly advances the art.
[0009] More specifically, since the receiver and transmitter
apertures are different and separated, they can now be of different
sizes. This is particularly advantageous when the transmitter
aperture is relatively small--being adapted for optical coupling
via a rather small beam deflector such as the scan mirror or
assembly.
[0010] Although the invention even as most broadly or generally
described represents a notable improvement, nevertheless it is
ideally practiced with certain preferred enhancements or options
that provide yet further benefits. For example, preferably the
receiver has an aperture that is larger than the transmitter
aperture.
[0011] Preferably the receiver aperture area is at least five times
that of the transmitter aperture. Ideally the receiver is a single
unitary module; however, if all constraints cannot be met in this
way, then the receiver preferably includes plural receiver modules
each having an aperture, and the aggregate aperture area of the
plural receiver modules is larger than the area of the transmitter
aperture; in this case further preferably the aperture area of each
one of the plural receiver modules is larger than the area of the
transmitter aperture.
[0012] Preferably the apparatus further includes a beam expander,
disposed between the laser and the mirror or mirrors, for
controlling the beam waist or divergence, or both, particularly at
the mirror or mirrors. In this case further preferably the expander
is adjustable and enables selection of Gaussian or Rayleigh
divergence, to effectively provide a "zoom" function.
[0013] Another preference is that the apparatus further include an
auxiliary optical system for calibrating the deflection produced by
the mirror or mirror assembly. If it does, then there are two
subpreferences:
[0014] (1) the laser beam follows a particular optical path at the
mirror or mirrors, and the auxiliary optical system includes:
[0015] means for causing an auxiliary radiation beam to follow, at
the mirror or mirrors, an optical path identical or similar to the
particular path, and [0016] means for monitoring deflection of the
auxiliary beam by the mirror or mirrors; and also
[0017] (2) the causing means include a beamsplitter for at least
roughly aligning the auxiliary beam with the laser beam in
approaching the mirror or mirrors.
[0018] In the case of this latter subpreference there is a group of
related and nested further preferences. Preferably: [0019] the
apparatus further includes some means for separating the auxiliary
beam from the laser beam after leaving the mirror or mirrors; and
an auxiliary detector for determining deflection of the separated
auxiliary beam by the mirror or mirrors; [0020] the apparatus
includes some means for correlating the determined deflection with
control signals that operate the mirror or mirrors; [0021] the
separating means include some means for passing the auxiliary beam
through the same beamsplitter again, or through another
beamsplitter; [0022] the auxiliary detector is a position-sensing
detector ("PSD"); [0023] a the beamsplitter is wavelength
sensitive; and the auxiliary beam and laser beam are of different
wavelengths; [0024] a the beamsplitter is a dichroic element;
[0025] a the beamsplitter is a holographic element; [0026] the
apparatus further includes some means for at least roughly
synchronizing pulses of the laser beam with sensitive times or
dispositions, or both, of the receiver (here it will be understood
that the term "disposition" encompasses location or orientation, or
both); [0027] the apparatus further includes one or both of: (a)
calculating means for determining time delay between transmission
of a pulse of the laser beam and receipt of a reflected return of
the pulse from an object, and (b) some comparison means for
determining Doppler shift in the laser beam; [0028] the calculating
or comparison means further include, respectively: some means for
calculating object distance from the determined time delay, or some
means for deriving relative speed from the shift; [0029] the
apparatus further includes some means for incorporating information
about the apparatus orientation or location, or both, together with
information that the apparatus has noticed a return from an object,
or distance of such an object, or both.
[0030] We also have certain other basic preferences: preferably the
receiver has a detector of particular overall dimensions, and is
controlled actively to select operation as either: [0031] a single
unit having said particular overall dimensions, or [0032] multiple
subsections of the detector, each having dimensions smaller than
said particular overall dimensions.
[0033] In either of these cases, a sampled region is selected based
on knowledge of where the scan mirror is pointing the laser, to
facilitate sampling of smaller units.
[0034] Preferably the apparatus further includes some means for
measuring the angles of beam deflection by the scan mirror or
mirror assembly; and the measuring means include: [0035] a
capacitive sensor responsive to an individual mirror or mirrors; or
[0036] a magnetic sensor responsive to an individual mirror or
mirrors; or [0037] a lookup table calibrated in drive voltage or
current supplied to an individual mirror or mirrors.
[0038] In its second main facet or aspect, too, the invention is
lidar apparatus. It includes a lidar transmitter having a laser
source that produces a laser beam, a scan mirror or scan-mirror
assembly angularly adjustable to deflect the beam in at least two
orthogonal directions; and an auxiliary optical system for
calibrating the deflection by the mirror or mirror assembly.
[0039] The foregoing may be a definition or description of the
second aspect of the invention in its broadest or most general
form. Even as thus broadly couched, however, it can be seen that
this facet of the invention significantly advances the art.
[0040] More specifically, the auxiliary optical train enables
closed-loop, real-time calibration of the deflections--so that
error in pointing accuracy is virtually eliminated even under many
circumstances that might degrade the reliability of precalibration,
e. g. at the factory.
[0041] Although the invention even as most broadly or generally
described represents a notable improvement, nevertheless the
invention is ideally practiced with certain preferred enhancements
or options that provide even further benefit. For example, given
that the laser beam follows a particular optical path at the mirror
or mirrors, we prefer that the auxiliary optical system include:
[0042] some means for causing an auxiliary radiation beam to follow
an identical or similar optical path at the mirror or mirrors, and
[0043] some means for monitoring deflection of the auxiliary beam
by the mirror or mirrors.
[0044] In this case it is further preferable that the causing means
include a beamsplitter for at least roughly aligning the auxiliary
beam with the laser beam in approaching the mirror or mirrors. If
this preference is observed, then it is still further preferable
that the apparatus also include: [0045] some means for separating
the auxiliary beam from the laser beam after leaving the mirror or
mirrors; and [0046] an auxiliary detector for determining
deflection of the separated auxiliary beam by the mirror or
mirrors.
[0047] If the apparatus does include these elements, then there are
three further preferences: [0048] a that the apparatus include some
means for correlating the determined deflection with control
signals that operate the mirror or mirrors, so that the correlated
signals provide a calibration of operation of the mirror or
mirrors; [0049] that the separating means include some means for
passing the auxiliary beam through the same beamsplitter or another
beamsplitter; and [0050] that the auxiliary detector be a
position-sensing detector ("PSD").
[0051] A still further preference is that the beamsplitter be
wavelength sensitive, and the auxiliary beam and laser beam be of
different wavelengths. Yet another is that the beamsplitter be a
dichroic element.
[0052] In its third main facet or aspect the invention is a method
for noticing and responding to a remote light source. The method
uses a transmitter that includes a local radiation source that
produces a laser beam, a scan mirror or scan-mirror assembly
angularly adjustable to deflect the beam in at least two orthogonal
directions--and an afocal optical unit for magnifying the beam
deflection. The transmitter has an aperture for transmitting the
beams and a radiation receiver that does not share the transmitter
aperture.
[0053] The method includes the step of operating the receiver to
notice and determine a location of the remote source. It also
includes the step of controlling the transmitter to direct the
laser beam back toward the determined location.
[0054] The foregoing may be a definition or description of the
third aspect of the invention in its broadest or most general form.
Even as thus broadly couched, however, it can be seen that this
facet of the invention significantly advances the art.
[0055] More specifically, by returning a response beam from the
transmitter to the source location, this aspect of the invention
takes advantage of both the potentially large-aperture receiver for
pinpointing the location, and the relatively smaller-aperture
transmitter suited to nimble beam steering with the scan mirror or
assembly.
[0056] Although the invention even as most broadly or generally
described represents a notable improvement, nevertheless the
invention is ideally practiced with certain preferred enhancements
or options that provide even further benefit. For example,
preferably the method further includes the step of activating the
receiver to collect and interpret reflected radiation of the
back-directed laser beam, received from the location. Another
preference is that the method further utilize the step of
activating an additional receiver to collect and interpret
reflected radiation of the back-directed laser beam, received from
the location.
[0057] Still another preference is that the first-mentioned
receiver and the additional receiver be sensitive in respective
different wavelength bands, namely: a first spectral waveband
encompassing emissions of expected remote sources including but not
necessarily limited to the remote light source; and a second
spectral waveband encompassing the laser beam. Yet another
preference is that the activating step include using the additional
receiver in a lidar operating mode to as determine return time of
the laser beam and thereby distance of a reflecting object at the
location.
[0058] All of the foregoing benefits and advantages will be more
clearly understood from the detailed description that follows, with
reference to the accompanying drawings--of which:
BRIEF DESCRIPTION OF THE DRAWINGS
[0059] FIG. 1 is a top plan, highly schematic, of the lidar
laser-projection and -reception optics, source and detector,
including the transmission field of regard ("FOR") and reception
FOR, and the outbound optical beams both inside and outside the
optical system--as well as an internal auxiliary alignment
beam--all integrated with a block diagram of the electronics and
other functional modules, conceptually including signals to and
from those modules;
[0060] FIG. 2 is a like view of the FIG. 1 optics only, and with
the optical paths and fields greatly simplified to show only the
main source beam;
[0061] FIG. 3 is a front elevation, also highly schematic, of the
FIGS. 1 and 2 optics;
[0062] FIG. 4 is a plan like FIGS. 1 and 2 but showing only the
reception optics, together with principal dimensional definitions
of the reception subsystem;
[0063] FIG. 5 is a detailed front elevation, also highly schematic,
of the detector that is part of the reception optics;
[0064] FIGS. 6 and 7 are views like FIGS. 2 and 3, respectively,
but with an additional receiver included in the system for purposes
to be described below;
[0065] FIG. 8 is a plan like FIGS. 1, 2, 6 and 7 but highly
schematic and very greatly enlarged--and showing only the mirror
back-plate and a single representative mirror, in some of its
various motions;
[0066] FIG. 9 is a flow chart particularly related to some
functions of the dual-receiver configuration of FIGS. 6 and 7;
and
[0067] FIG. 10 is a plan like FIG. 6 but for a variant.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0068] A reflective element or module 3 (FIGS. 1 and 2)--which can
be a small, single mirror, or a MEMS scan mirror, or a MEMS
scan-mirror array--can be used for projection but not for capturing
the reflected beam. As in previous work of Bowker, Lubard and
McLean, as well as our own earlier innovations mentioned above, it
is possible to accumulate data that give, in effect, a
three-dimensional impression of a region by aggregating numerous
two-dimensional or flying-spot data elements.
[0069] The lidar system includes an afocal MEMS beam-steering
(AMBS) transmitter TX (FIGS. 1, 2 and 4), and a receiver RX. The
AMBS transmitter system (hereinafter "AMBS-TX") and the receiver
system address a common field of regard ("FOR"), with angular
extent .theta..sub.FOR, about the X and Z axes (FIGS. 3 and 5).
More precisely, the angles .theta. (FIG. 1) that are actually shown
represent horizontal angular position .theta..sub.x; whereas the
orthogonal angles representing vertical angular position
.theta..sub.z are in and out of the plane of the paper.
[0070] The AMBS-TX directs a lidar laser beam to a field location
of interest, where the beam is reflected by an object 30 if
present. The reflected light, if any, is collected by the receiver
RX. The location of an object in the X, Y, Z coordinate system
relative to the lidar transceiver is determined by measuring
distance D to the object and the vertical and horizontal angular
positions .theta..sub.z, .theta..sub.x of the laser reflection from
the object. Lasers in various embodiments operate either pulsed or
CW. Distance to the object is characterized by one or both of two
methods: [0071] 1) Actual distance as such equals time of flight
for pulsed laser light to leave the AMBS-TX and return to the
receiver, times the speed of light, divided by two. [0072] 2) The
first time derivative of the distance is ascertained from observed
Doppler shift in amplitude-modulated CW laser-radiation frequency
that occurs when the lidar laser radiation is reflected from the
object and sensed by the detector. The latter information is
particularly useful when the camera-style lidar setup of our
invention is incorporated into or associated with a
rendezvous-and-docking system or a collision-avoidance
system--whether for spacecraft or automobiles, or otherwise--or any
other sort of situation in which it is desired to know speed of
approach or speed of recession.
[0073] Horizontal and vertical angular positions .theta..sub.x,
.theta..sub.z of the object, relative to the AMBS-TX, are
determined by one or both of two additional methods: [0074] 1)
Knowledge of the MEMS scan-mirror angles .phi..sub.x and
.phi..sub.z is related to the projected lidar laser-beam horizontal
and vertical angular positions .theta..sub.x, .theta..sub.z-based
on the MEMS reflection geometry and afocal-lens magnification M.
(Here again the actually illustrated angles .phi., M.phi. [FIG. 1]
represent the horizontal angular positions e. g. .phi..sub.x, while
the orthogonal angles representing vertical angular position
.phi..sub.z are in and out of the plane of the paper.) For
simplicity of this document, the afocal magnifier 4 is herein
called a "lens assembly" or "lens", but it is to be understood that
this afocal element may instead be another type of refractor, or a
reflector, or a combination or hybrid refractor/reflector. [0075]
2) Knowledge of where in the detector X-Z image plane 6 (FIG. 5),
the image 42 of the laser reflection from the object is imaged is
related geometrically to the focal length f (FIG. 4) of the
receiver lens 4 and the corresponding X, Z object location.
[0076] The smallest resolvable angular extent or subtense of the
lidar beam 31 about horizontal and vertical angular positions
.theta..sub.x and .theta..sub.z is determined by one of these
conditions: [0077] 1) the lidar laser beam divergence
.theta..sub.DIV--if .theta..sub.DIV.ltoreq.p/f, where p is the
minimum sample size of the receiver detector 6 and f is the focal
length of the receiver lens 4; and otherwise [0078] 2) p/f (i. e.
if .theta..sub.DIV>p/f). For a single receiver module, in
angular measure the FOR at the receiver .theta..sub.FOR is
established by the optical relationships (FIG. 5) at the
detector:
[0078] tan ( 1 2 .theta. FOR - RX ) = W 2 f , ##EQU00001##
or in other words
.theta. FOR - RX = 2 arctan W 2 f . ##EQU00002##
The lidar system includes the following major elements. [0079] 1)
The lidar laser 1 operates at a wavelength .lamda..sub.1 and is
controlled 21 by a central processor 11 to synchronize the laser
pulse 34, 35 with the MEMS scan mirror 3--in order to address the
desired horizontal and vertical angular positions .theta..sub.x and
.theta..sub.z. The scan mirror or array 3 is supported by a
substrate 38. The laser beam 34, 35 passes through a beam-expander
lens 2 and then a dichroic beamsplitter 8, reflects from the MEMS
scan mirror 3 and then passes again 36 through a different part of
the splitter 8 and through an afocal lens assembly 4 for
transmission 31 to the object 30. [0080] 2) The beam expander 2
controls the laser divergence and beam waist at the MEMS scan
mirror 3. The option to allow for Gaussian or Rayleigh divergence
.theta..sub.DIV may be made selectable, allowing for a nearly
two-times change in divergence; this is in effect a "zoom"
capability:
[0080] a . .theta. DIV .about. 4 .lamda. .pi. d MEMS , Gaussian
divergence ; ##EQU00003## b . .theta. DIV .about. 2.44 .lamda. .pi.
d MEMS , Rayleigh divergence . ##EQU00003.2## [0081] 3) The
two-axis HEMS scan mirror 3 directs the lidar laser beam about
horizontal and vertical angular positions .theta..sub.x and
.theta..sub.z. This mirror steers the beam 36 in angle
.phi..sub.MEMS relative to the optical axis 32. [0082] 4) The
afocal lens assembly 4 is used to magnify the angular field of
regard .theta..sub.FOR-TX (FIG. 1) that can be addressed by the
lidar laser beam. The afocal lens assembly magnification M:1
results in a laser horizontal or vertical angular position angle of
M.phi..sub.MEMS. The laser-beam divergence, too, is increased by
the angular magnification M--so that beyond the afocal lens
assembly 4 the divergence is now:
[0082] a . .theta. DIV .about. 4 M .lamda. .pi. d MEMS , Gaussian
divergence ; ##EQU00004## b . .theta. DIV .about. 2.44 M .lamda.
.pi. d MEMS , Rayleigh divergence . ##EQU00004.2## [0083] 5) A
receiver lens 5 intercepts returning laser reflection from the
object 30--within the receiver field of regard .theta..sub.FOR-RX
(most typically centered on an optical axis 33 of the
receiver)--and focuses it on the detector 6 (FIGS. 1, 4 and 5).
[0084] 6) The detector senses the lidar laser beam reflected by the
object, and thereby measures the object distance D and relative
speed (whether for rendezvous or preventing collision)--based on
time of flight or Doppler shift, respectively, as mentioned
earlier. When the detector senses the return, the CPU 11 or lidar
processor 12 notices the signal and also detects the corresponding
MEMS scan angles .phi..sub.x and .phi..sub.z and thus the
field-location angles .theta..sub.x and .theta..sub.z. The detector
can be a single unit of dimensions W by W (FIG. 5) or can be
composed of multiple subsections of dimensions p by p.
Advantageously the detector-unit size is controlled actively,
determining the sampled region based on knowledge of where the scan
mirror is pointing the laser beam. This allows for
addressing/sampling of smaller units--e. g. pixels of interest, a
subset of the entire array, as opposed to the entire detector
array. Such small-unit sampling lowers the capacitance and
resistance associated with the effective detection unit, and
thereby provides the highest possible sampling rate. [0085] 7) An
auxiliary, MEMS-calibration light source 7 operating at
.lamda..sub.2 reflects at the dichroic beamsplitter 8, to travel
along the same path 36 as the lidar laser source 1 operating
.lamda..sub.1. After reflection by the MEMS scan mirror, the
auxiliary beam 27 is again reflected from the beamsplitter 8 and
directed to a two-axis position-sensing detector ("PSD") or any
other detector 9 enabling measurement of the MEMS-mirror scan angle
.phi..sub.MEMS. [0086] 8) The spatial separation of radiation
beams--namely, the separation needed to establish the congruent
beam paths 36, 27 within the central optical system but diverging
optical paths outside that region--is based upon wavelength
discrimination by the dichroic beamsplitter. It transmits the lidar
laser beam of one wavelength .lamda..sub.1 but reflects the
auxiliary calibration beam of a different wavelength .lamda..sub.2.
Also within the scope of the invention is an alternative
configuration in which .lamda..sub.1 is reflected and .lamda..sub.2
transmitted. [0087] 9) The two-axis PSD 9 intercepts the auxiliary
beam after reflection by the scan mirror 3. Output signals from the
PSD provide information on the MEMS scan angle, and thus the
lidar-laser horizontal and vertical angular-position values
.theta..sub.z and .theta..sub.x--as well as providing feedback for
closed-loop control, of the scan mirror. The scan angle of that
mirror can be found from a lookup table ("LUT") based on the known
function of angle vs. voltage (or instead vs. current or
capacitance, or magnetic state) of the MEMS actuators, or can be
found from the built-in optical calibration detailed in paragraphs
7 through 9 above. Alternatively this built-in calibration can be
used to construct (or after possible damage or disruption
reconstruct) the LUT for subsequent quick reference. Again, the
scan-mirror angles .phi..sub.x and .phi..sub.z and thus (given M)
field-location angles .theta..sub.x and .theta..sub.z can be
learned by measuring the voltages or currents applied to the MEMS
actuators, or based on capacitance or magnetic-field sensor outputs
which relate those properties to the corresponding angles, once
such an LUT has been generated. If any of these approaches is used,
then for measurement of .phi..sub.x and .phi..sub.z it is not
necessary to include any of the second laser source 7, dichroic
mirror/splitter 8, and detector 9. [0088] 10) A programmed
general-purpose central processor 11 controls 21 pulsing of the
laser 1 and also controls and monitors 24 sensitivity of the
detector 6, to enable generally synchronous detection--with
allowance for the time lags needed in basic lidar operation. The
processor 11 also interacts 23 with the PSD 9, and can set 22 the
orientation of the mirror substrate panel 38, as one means of
presetting the mirror(s) 3 calibration. [0089] 11) A secondary,
special-purpose lidar processor 12 provides the above-mentioned
basic lidar operation, providing precise intersignal timing 25, 26
that enables the apparatus to first: [0090] a. "notice" receipt of
an optical-return signal 26 nominally synchronous with a lidar
trigger signal 25 and a corresponding output pulse 34, 31; and then
[0091] b. based on the intersignal timing, determine the "distance"
of an object 30 responsible for the return. [0092] 12) An
orientation and a location module 13, 14 simply enable the system
to incorporate its own orientation and location (collectively
"disposition") into information read out to human users or for
automatic response, as may be the case. Orientation and location
may be based on sightings to fixed or known-location stations,
followed e. g. by triangulation. If preferred, they may instead be
inferred from feedback signals of conventional spinning-mass
devices, or location found by a global-positioning unit. These
diverse kinds of data source can be mixed and matched as desired.
The system can report its raw angular determinations separately
from the disposition, for integration elsewhere; however, if
preferred the system 11-14 can preintegrate the disposition into
the lidar data to produce e. g. geodetic coordinates for the
objects noticed by the system. [0093] 13) The aperture of the
deflecting mirror subsystem 3 is both necessarily and
advantageously (for purposes of transmitting a very intense beam
that initially is tightly collimated) quite small. Correspondingly
the apertures elsewhere in the transmission system TX--particularly
including the aperture 4' of the afocal assembly 4--are all also
small. For detection purposes, on the other hand, particularly with
a weak return, it is desirable to collect as much light as
possible. Since the present invention is particularly distinguished
by separate (i. e., not shared-aperture) transmission and reception
systems TX, RX, it is not necessary in this system to make the
receiver aperture 5' the same size as the final transmission
aperture 4'. Therefore, merely by way of example, the afocal-lens
aperture diameter 4' may be advantageously in the range of 0.1 to
10 mm; while the receiver aperture diameter 5' may be
advantageously in the range of 10 to 50 mm. These values vary
widely with the application at hand. For further optimization it is
also possible to provide plural receiver modules RX to cover the
full FOR of the transmitter TX with its magnifying afocal optical
assembly 4. [0094] 14) The entire apparatus, including the
processor and related modules 11-14, may be housed together in a
common case. Alternatively if preferred the transmitter TX and
receiver RX units may be held in a smaller case 37 (FIGS. 1 through
3), and the processor etc. modules 11-14 packaged separately--with
the signal links 21-26 provided by e. g. radio signals or cabling.
As will be understood, these choices are a matter of economic
constraints, convenience, or requirements imposed by size and
weight limitations for the application at hand.
[0095] When searching for a source location, the system can simply
determine the "point" (i. e., focused spot) location directly if
the laser-beam divergence is smaller than the receiver per-pixel
FOV ("PPFOV"). If it is not, then for better angular measurement
the system can fit to the centroid of the return. It will be
understood that most commonly the interest is not in the shape as
such, but rather only in using it as a means for improving position
accuracy.
[0096] An advantageous variant configuration of the invention
includes an additional receiver 105 (FIGS. 6 and 7), with its own
respective optical axis 105' and imaging detector 106. Preferably
one of the two RX units 5, 105 is particularly sensitive at the
wavelength or wavelengths emitted by the laser 1, for use in a
lidar, or "active", mode to measure the distance of noticed
objects.
[0097] The other of the two RX units is for use in a "passive", or
nonlidar, mode for noticing self-luminous objects--i. e., radiation
sources--and accordingly is sensitive over a wavelength band in
which such sources are generally expected to be emitting. Either or
both receivers may be adapted for certain kinds of wavelength
measurements too, so that they can be used for Doppler measurements
to measure the speed of the noticed device.
[0098] Thus with the dual-receiver form of the invention, the
system can first notice 71 (FIG. 9) a remote source by passive
detection at the passive-mode receiver, and analyze the
corresponding image position on the detector plane to locate 72 the
source in the field domain. Given that location, the system can
then reply 73 with a pulse of light from laser 1, returned to that
source location.
[0099] If an object at the source reflects the reply pulse, the
system can then receive 74 the reflected pulse at the active-mode
receiver, and based upon timing relative to the outgoing laser
pulse can interpret 75 the relationships to measure the
source-object distance. As an alternative, or in addition, to lidar
measurement the outgoing pulse can be caused to amplitude-overload
optical equipment or personnel, or otherwise to jam operations, at
the source--but this would not normally be appropriate in use of
the invention for collision avoidance or docking.
[0100] An individual MEMS mirror conventionally has a rest position
63 (FIG. 8) that is generally parallel to the back-plane 38 of the
mirror or array. By operation of electrically driven conventional
actuators, not shown, each mirror undergoes rotation 64 (within the
plane of the drawing, and also other rotation not shown that is in
and out of the drawing plane) to rotated positions e. g. 63'.
[0101] In preferred embodiments of our invention, each mirror also
undergoes independent translation 65 in a so-called "piston"
direction to adopt dispositions e. g. 63''. The magnitudes and
directions of these motions can be determined from the voltage and
current directed to the actuators, and as noted earlier these drive
signals can be calibrated and the calibration memorized in a lookup
table so that the deflections and corresponding field positions at
each moment can be found automatically by finding their
instantaneous values in the table.
[0102] An alternative technique for rapid determination of the
mirror disposition is to measure it with calibrated sensors 66.
These can be capacitive, magnetic, optical, acoustic etc.
[0103] As detailed above, some preferred embodiments of our
invention have receiver-aperture area that is individually larger
than the transmitter-aperture area. In a variant preferred
configuration, individual receiver-apertures 205' (FIG. 10), 305'
have respective aperture areas individually smaller--but in the
aggregate larger--than the transmitter-aperture area 4. As will be
understood by people of ordinary skill in this field, the plural
receiver apertures 205', 305' can be multiple apertures, i. e.
three, four or more apertures.
[0104] The foregoing descriptions are intended to be, and are,
merely exemplary, not to limit the scope of the invention--which is
to be determined solely by reference to the appended claims.
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