U.S. patent application number 17/367913 was filed with the patent office on 2022-02-03 for efficient control system and method for brushless motor with wide working range.
This patent application is currently assigned to Zhejiang University. The applicant listed for this patent is Zhejiang University. Invention is credited to Junyin Chen, Changping Du, Guanghua Song, Rui Yang, Zhixian Ye, Zekun Zhang, Yao Zheng.
Application Number | 20220032786 17/367913 |
Document ID | / |
Family ID | |
Filed Date | 2022-02-03 |
United States Patent
Application |
20220032786 |
Kind Code |
A1 |
Zheng; Yao ; et al. |
February 3, 2022 |
Efficient Control System and Method For Brushless Motor With Wide
Working Range
Abstract
The present disclosure provides an efficient control system and
method for a brushless motor with a wide working range, which are
applied to an aerospace vehicle energy system. The system of the
present disclosure includes a power supplying module, a first DC-DC
circuit, a battery pack, a second DC-DC circuit, an
anti-reverse-connection circuit, an electronic speed control (ESC),
a brushless direct current motor (BLDC), an airborne controller and
a communication link. Electric energy from the power supplying
module is configured to charge the battery pack via the first DC-DC
circuit, and electric energy of the battery pack sequentially flows
through the second DC-DC circuit and the anti-reverse-connection
circuit to energize the ESC, wherein output voltage of the second
DC-DC circuit and throttle signal input of the ESC are controlled
in real time by the airborne controller according to a power demand
of an aircraft.
Inventors: |
Zheng; Yao; (Hangzhou,
CN) ; Chen; Junyin; (Hangzhou, CN) ; Du;
Changping; (Hangzhou, CN) ; Song; Guanghua;
(Hangzhou, CN) ; Yang; Rui; (Hangzhou, CN)
; Ye; Zhixian; (Hangzhou, CN) ; Zhang; Zekun;
(Hangzhou, CN) |
|
Applicant: |
Name |
City |
State |
Country |
Type |
Zhejiang University |
Hangzhou |
|
CN |
|
|
Assignee: |
Zhejiang University
Hangzhou
CN
|
Appl. No.: |
17/367913 |
Filed: |
July 6, 2021 |
International
Class: |
B60L 50/52 20060101
B60L050/52; B60L 50/60 20060101 B60L050/60; H02P 7/292 20060101
H02P007/292 |
Foreign Application Data
Date |
Code |
Application Number |
Jul 28, 2020 |
CN |
202010739605.8 |
Claims
1. An efficient control method for a brushless motor with a wide
working range, comprising: at a system including a power supplying
module, a first DC-DC circuit, a battery pack, a second DC-DC
circuit, an anti-reverse-connection circuit, an electronic speed
control (ESC), a brushless direct current motor (BLDC), an airborne
controller, a communication link, wherein the power supplying
module outputs regulated direct currents to energize the battery
pack through the first DC-DC circuit; wherein the battery pack
energizes the ESC through the second DC-DC circuit and the
anti-reverse-connection circuit in sequence, and the ESC drives the
BLDC to rotate; wherein the second DC-DC circuit uses an adjustable
DC-DC circuit, which changes an output voltage according to an
input signal; wherein the communication link is configured to
transmit an original throttle signal output by a flight control
system to the airborne controller; and wherein the airborne
controller is configured to acquire input/output voltage and
current information from the first DC-DC circuit and output voltage
and current information of the battery pack for monitoring, make
the original throttle signal transmitted from the communication
link correspond to a power demand of a power system, output two
control signals according to a relationship between a power demand
of a current aircraft and a set power threshold, and a first
control signal is output to the ESC for controlling throttle thrust
of the ESC, and a second control signal is output to the second
DC-DC circuit for controlling the second DC-DC circuit to output a
matched voltage: receiving, by the airborne controller, the
original throttle signal output by the flight control system via a
communication link, and mapping the original throttle signal to the
power demand of the power system so as to obtain the power demand
of the power system at a current time point; and determining the
power demand of the power system, including: when the power demand
of the power system is less than or equal to a preset power
threshold, outputting, by the flight control system, the control
signal of the ESC to change an actual throttle value, and
simultaneously controlling, by the airborne controller, the second
DC-DC circuit to energize with a reference voltage, the reference
voltage being the lowest voltage output by the second DC-DC circuit
that is the lowest voltage supported by the ESC; and when the power
demand of the power system is greater than the preset power
threshold, simultaneously changing, by the airborne controller, the
throttle thrust of the ESC and the output voltage of the second
DC-DC circuit according to a joint adjustment strategy so as to
realize high-power power output,
2. The efficient control method for a brushless motor with a wide
working range according to claim 1, wherein the system further
comprises a voltage regulation module for providing a stable power
supply for an airborne apparatus.
3. The efficient control method for a brushless motor with a wide
working range according to claim 1, wherein the power supplying
module includes photovoltaic energization, fuel cell energization
and fuel generator energization, with single-channel energization
or multi-channel parallel energization.
4. The efficient control method for a brushless motor with a wide
working range according to claim 1, wherein the first DC-DC circuit
and the second DC-DC circuit are a BUCK-type circuit or a
BUCK-BOOST-type circuit.
5. The efficient control method for a brushless motor with a wide
working range according to claim 1, wherein the joint adjustment
strategy consults a pre-obtained power matching table, so as to
output the throttle thrust of the ESC and the output voltage of the
second DC-DC circuit corresponding to demanded power, wherein the
power matching table records an operating voltage and the throttle
thrust of the ESC corresponding to an optimal efficiency of the
system under different power demands.
6. The efficient control method for a brushless motor with a wide
working range according to claim 5, wherein the power matching
table is obtained through a wind tunnel test by firstly obtaining
an efficiency curve of a power device with equal power output under
a target working condition, and then recording the operating
voltage and the throttle thrust corresponding to a highest
efficiency point on the efficiency curve one by one, and recording
an operating voltage, the throttle thrust and power corresponding
to a highest point in each efficiency curve so as to obtain the
power matching table, different equal power outputs respectively
corresponding to respective efficiency curves.
7. The efficient control method for a brushless motor with a wide
working range according to claim 1, wherein the joint adjustment
strategy includes additionally mounting a corresponding force
sensor on a power system and incorporating a dynamic tracking
algorithm to track the highest real-time efficiency of the power
system.
8. The efficient control method for a brushless motor with a wide
working range according to claim 1, wherein the mapping the
original throttle signal to the power demand of the power system
uses linear mapping.
Description
CROSS REFERENCE TO RELATED APPLICATIONS
[0001] This patent application claims the benefit and priority of
Chinese Patent Application No. 202010739605.8 filed on Jul. 28,
2020, the disclosure of which is incorporated by reference herein
in its entirety as part of the present application.
TECHNICAL FIELD
[0002] The present disclosure pertains to the technical field of
aerospace vehicle energy systems, and particularly relates to an
efficient control system and method for a brushless motor with a
wide working range.
BACKGROUND
[0003] For some specific brushless power systems (such as a
long-endurance electric Unmanned Aerial Vehicle (UAV) and a tilting
electric UAV capable of vertical taking-off and landing) a working
range is required to be wide. However, it is difficult to achieve
efficient power output in a wide working range through a
traditional constant-voltage drive control method. For example, for
the long-endurance electric UAV, the power required during a cruise
phase is low, which is lower than 1/4 of a rated power of a
brushless direct current motor (BLDC), and deviates from a high
efficiency section of the power system. When it comes to the
tilting electric UAV capable of vertical taking-off and landing,
the same set of power unit is adopted for vertical take-off and
horizontal cruise, and a required power value difference between
these two operating states is huge. If the conventional
constant-voltage drive method is used, an operating voltage for the
system is usually determined by satisfying the requirements of
vertical takeoff, which leads to low efficiency of the power system
when the UAV is flying horizontally.
SUMMARY
[0004] The present disclosure advantageously provides an efficient
control system and method for a brushless motor with a wide working
range against the deficiencies in the prior art. The present
disclosure can realize power output within a certain voltage range
by means of a battery pack connected in series with a DC-DC
circuit, and jointly adjust and control an input voltage of an
Electronic Speed Control (ESC) and throttle input of the ESC
through a corresponding control strategy, thereby improving overall
efficiency of a power system, and realizing efficient output of the
system within a wide working range.
[0005] The present disclosure is implemented with the following
technical solutions.
[0006] An efficient control system for a brushless motor with a
wide working range includes a power supplying module, a first DC-DC
circuit, a battery pack, a second DC-DC circuit, an
anti-reverse-connection circuit, an ESC, a brushless direct current
motor (BLDC), an airborne controller and a communication link,
wherein the power supplying module outputs regulated direct
currents to energize the battery pack through the first DC-DC
circuit; wherein the battery pack energizes the ESC through the
second DC-DC circuit and the anti-reverse-connection circuit in
sequence, and the ESC drives the BLDC to rotate; wherein the second
DC-DC circuit uses an adjustable DC-DC circuit which can change an
output voltage according to an input signal; wherein the
communication link is configured to transmitting an original
throttle value output by a flight control system to the airborne
controller; and wherein the airborne controller can acquire
input/output voltage and current information from the first DC-DC
circuit and output voltage and current information of the battery
pack for monitoring, make the original throttle value transmitted
from the communication link correspond to a power demand of a power
system, output two control signals according to a relationship
between a power demand of a current aircraft and a set power
threshold, and a first control signal is output to the ESC for
controlling throttle thrust of the ESC, and a second control signal
is output to the second DC-DC circuit for controlling the second
DC-DC circuit to output a matched voltage.
[0007] Furthermore, in the above technical solution, the system
further includes a voltage regulation module for providing a stable
power supply for an airborne apparatus.
[0008] Further, the power supplying module is implemented by
photovoltaic energization, fuel cell energization and fuel
generator energization, and single-channel or multi-channel
parallel energization can be adopted.
[0009] Further, the first DC-DC circuit and the second DC-DC
circuit may be a BUCK-type circuit, a synchronous BUCK-type circuit
or a BUCK-BOOST-type circuit.
[0010] An efficient control method for a brushless motor with a
wide working range is implemented based on the above system. The
control method includes receiving, by the airborne controller, the
original throttle signal output by the flight control system via a
communication link, and mapping the original throttle signal to the
power demand of the power system so as to obtain the power demand
of the power system at a current time point; and determining the
power demand of the power system: when the power demand of the
power system is less than or equal to a preset power threshold,
outputting, by the airborne controller, the control signal of the
ESC to change an actual throttle value, and simultaneously
controlling, by the airborne control system, the second DC-DC
circuit to energize with a reference voltage; and when the power
demand of the power system is greater than the preset power
threshold, simultaneously changing, by the airborne controller, the
throttle thrust of the ESC and the output voltage of the second
DC-DC circuit according to a joint adjustment strategy so as to
realize high-power power output.
[0011] In the above control method, the reference voltage is the
lowest voltage of actually output by the second DC-DC circuit, that
is, the lowest voltage supported by the ESC.
[0012] Further, the joint adjustment strategy is to consult a
pre-obtained power matching table, so as to output throttle thrust
of the ESC and an output voltage of the second DC-DC circuit
corresponding to demanded power, and the power matching table
records an operating voltage and throttle thrust of the ESC
corresponding to the optimal efficiency of the system under
different power demands. Still further, the power matching table
may be obtained through a wind tunnel test by obtaining an
efficiency curve of a power device with equal power output under a
target working condition firstly, and then recording an operating
voltage and throttle thrust corresponding to the highest efficiency
point on the curve one by one, and recording an operating voltage,
the throttle thrust and power corresponding to the highest point in
each efficiency curve so as to obtain the power matching table,
different equal power outputs respectively corresponding to
respective efficiency curves.
[0013] Alternatively, the joint adjustment strategy may be a
dynamic tracking algorithm aiming at tracking the highest real-time
efficiency of the power system by additionally mounting a
corresponding force sensor on a power system, which can be found in
CN 108791819A.
[0014] Further, the mapping the original throttle signal to a power
demand of a power system may use linear mapping to uniquely map the
original throttle signal to a power interval.
[0015] Compared with the prior art, the present disclosure has
obtained the following beneficial effects.
[0016] The present disclosure overcomes the defects of simplex
operating point and low efficiency at non-design points in a
conventional constant-voltage and variable-throttle-thrust control
method of brushless motor. The solution design of the present
disclosure innovatively controls the power system based on the idea
of variable voltage and variable throttle thrust. Specifically, the
input voltage and throttle signal of the ESC may be jointly
adjusted and controlled according to a given power demand, so that
the system can output efficiently under a wide working range,
wherein the working range refers to a power range within which the
power system may output the power efficiently, and the wide working
range means that the power system may output power efficiently in a
wide power range. Although the traditional constant-voltage and
variable-throttle-thrust scheme may realize from zero to maximum
power output of a current operating voltage, the efficiency of the
system is often not high when deviating from a rated power value,
and therefore cannot be considered as operating under the so-called
wide working range as referred in the present disclosure. The
technical effects of the present disclosure may be proved by FIG.
3. FIG. 3 is an efficiency diagram of a power system with equal
power output of 60 W. The operating state of 60 W output is
analyzed, and for the power system of this embodiment, if the
conventional brushless motor control system is adopted, an
operating voltage within 22-25 V is usually adopted to guarantee to
achieve maximum power output of the system as well as match an
actual voltage range of the battery pack. It may be seen from the
figure that under this operating voltage, the efficiency of the
power system is about 69%, and with the solution of the present
disclosure, the operating voltage of the power system may
accurately match an optimal operating voltage of 12.2 V. At this
time, the efficiency of the power system is 80.5%, which is 16.67%
higher than that of the conventional solution.
[0017] In addition, the present disclosure is based on the creative
idea of brushless motor control with the variable voltage and
variable throttle thrust, which not only enables the battery pack
to supply power to the ESC with a specific voltage so as to satisfy
power output within a certain power range, but also supplies power
to the ESC only via the adjustable DC-DC circuit when the system
needs to output at other power values. Compared with the above
solution, the present disclosure is improved in the following
aspects. If the battery pack is configured to directly supply
power, it usually may not accurately match an optimal voltage value
due to voltage characteristics of the battery pack. For example, a
lithium battery pack having fully charged at 12.6 V has a voltage
in a range of 10.5 V-12.6 V in an operating state, while an
operating voltage corresponding to an actual optimal efficiency
point may be 11.5 V. That is to say, it will deviate from the
optimal operating point. The actual operating voltage is not the
optimal operation voltage if the battery pack is configured as
direct power supply. This is the case especially when the
efficiency curve of the system presents an obvious peak during
equal power output. However, when the solution of the present
disclosure is adopted, the second DC-DC circuit supplies power to
the ESC regardless of the actual voltage of the battery pack, which
may guarantee that the operating voltage of the system is always at
a relatively accurate value (that is, the optimal operating voltage
in the power matching table mentioned in the present disclosure),
and further guarantee the system efficiency.
[0018] The solution of the present disclosure is designed to be
highly applicable for the practical application objects, and may be
realized by retrofitting the existing traditional solution and
adding the adjustable DC-DC circuit and the airborne controller
module.
[0019] The control over brushless motor with a wide working range
is based on the considerations as follows. Specifically, in the
traditional solution, for various power supplying modules, such as
a photovoltaic module, a fuel cell and a fuel power generation
device, a battery pack with a relatively high voltage is usually
connected thereafter to meet a demand of high power output of the
power system. Based on the solution of the present disclosure, the
battery pack in the traditional solution does not need to be
replaced, and the adjustable DC-DC circuit and the airborne
controller may be directly added to original circuit wiring to
upgrade the original scheme, so as to improve a performance of the
power system, and enable the efficient system power output in a
wide working range.
BRIEF DESCRIPTION OF THE DRAWINGS
[0020] FIG. 1 is a structural schematic diagram of an efficient
control system for a brushless motor with a wide working range
according to the present disclosure;
[0021] FIG. 2 is a workflow chart of the efficient control system
for a brushless motor with a wide working range according to the
present disclosure; and
[0022] FIG. 3 is an equal power output system efficiency curve
(equal power output of 60 W) for creating a power matching
table.
[0023] Reference numerals in the figures include 1--power supplying
module; 2--first DC--DC circuit; 3--battery pack; 4--second DC--DC
circuit; 5--anti-reverse-connection circuit; 6--(electronic speed
control) ESC; 7--brushless direct current motor (BLDC); 8--airborne
controller; 9--communication link; and 10--voltage regulation
module.
DETAILED DESCRIPTION
[0024] The present disclosure will be further described below with
reference to accompanying drawings and in conjunction with
particular embodiments.
[0025] As shown in FIG. 1, this embodiment mainly provides an
efficient control system for a brushless motor with a wide working
range, which includes a power supplying module, a first DC-DC
circuit, a battery pack, a second DC-DC circuit, an
anti-reverse-connection circuit, an electronic speed control (ESC),
a brushless direct current motor (BLDC), an airborne controller, a
communication link and a voltage regulation module.
[0026] The power supplying module energizes the battery pack via
the first DC-DC circuit. The power supplying module may be
configured to be implemented by photovoltaic energizing, fuel cell
energizing or fuel generator energizing, in the form of
single-channel or multi-channel parallel energizing. In a
particular embodiment, if the power supplying module is configured
as a photovoltaic module for supplying power, due to special I-V
characteristics of a photovoltaic cell, an MPPT controller, that
is, a maximum power point tracking controller, is usually added
between the power supplying module and the first DC-DC circuit, for
adjusting circuit parameters to achieve maximum power output of the
photovoltaic module. If the power supplying module is configured as
a fuel cell for supplying power, since power generation efficiency
of the fuel cell is related to the magnitude of its output voltage,
the fuel cell is usually set at a rated voltage to achieve
efficient output of a fuel cell stack. At this time, the first
DC-DC circuit is configured as a DC voltage regulation unit and
charges the battery pack. If the power supplying module is
configured as a fuel generator for supplying power, an output
voltage is unstable due to fluctuation of the speed of an engine,
and the first DC-DC circuit is also used for DC voltage regulation
and charges the battery pack. The first DC-DC circuit may be
configured as a BUCK-type circuit, a synchronous BUCK-type circuit
or a BUCK-BOOST-type circuit, such as an LM2577 boost digital
display module, a DSN6000AUD automatic buck-boost module, an LM317
buck circuit board and an AP-D5830A adjustable buck module.
[0027] Electric energy of the battery pack sequentially flows
through the second DC-DC circuit and the anti-reverse-connection
circuit to supply power for the ESC, and the ESC drives the BLDC to
rotate. The second DC-DC circuit is an adjustable DC-DC circuit,
which changes an output voltage according to an input signal, and
may be configured as the BUCK-type circuit, the synchronous
BUCK-type circuit or the BUCK-BOOST-type circuit, such as
AP-D5830A. The DC-DC buck module outputs constant-voltage DC with
an external voltage and current analog signal input terminal, and a
single-chip microcomputer may be configured to control and adjust
voltage and current. The anti-reverse-connection circuit is mainly
configured to prevent reverse connection, which may be a
conventional anti-reverse-connection circuit, such as a low-dropout
ideal diode with a maximum operating current of 15 A from Maikesi.
During conduction, voltage drops across a metal-oxide-semiconductor
field effect transistor (MOSFET) are only 20 mV. A 100V 50A ideal
diode from Jiadi may also be adopted, of which a static operating
current is 0.6-1.5 mA, design of dual metal oxide semiconductors
(MOS) is used and internal conduction resistance is merely 0.75
milliohm. Alternatively, the anti-reverse-connection circuit is
configured to include at least one MOS transistor and a diode
controller, the MOS transistor internally includes at least one
diode, a source (S) electrode of the MOS transistor is arranged at
an input terminal of the anti-reverse-connection circuit, a drain
(D) electrode of the MOS transistor is arranged at the output
terminal of the anti-reverse-connection circuit, an input terminal
of the diode controller is connected to the S electrode of the MOS
transistor, an output terminal of the diode controller is connected
to the D electrode of the MOS transistor, and a driving terminal of
the diode controller is connected to the gate (G) electrode of the
MOS transistor.
[0028] The communication link is configured to transmit an original
throttle value output by a flight control system to the airborne
controller.
[0029] A main control chip of the airborne controller may be
configured as stm32, 51, AVR, PIC and other types of single-chip
microcomputers, and cooperate with a corresponding peripheral
circuit, such as a voltage and current sensor--LTC2944 voltage and
current measurement module, which may acquire input/output voltage
and current information from the first DC-DC circuit and output
voltage and current information of the battery pack for monitoring
in real time, may make the original throttle value transmitted from
the communication link correspond to a power demand of a power
system, and output, according to a relationship between a power
demand of a current aircraft and a preset power threshold, a first
control signal to the ESC for controlling throttle thrust of the
ESC, and a second control signal to the second DC-DC circuit at the
same time for outputting a matched voltage value. The preset power
threshold may generally be set by those skilled in the art
according to experience or task requirements, for example, 15% of
maximum continuous operating power of the power system may be set
in the case of no experience or no specific task requirements. As
in a particular embodiment, the maximum continuous operating power
of the power system is 200 W, then the power threshold may be set
at 15% of 200 W, that is, 30 W.
[0030] The voltage regulation module is configured to provide a
stable power supply for an airborne apparatus, and may adopt an
integrated circuit to convert the output voltage of the battery
pack into 12 V voltage or 5 V voltage through an LT8632 chip. The
voltage regulation module is provided with protection circuits such
as a filter circuit and an isolation circuit, so as to stabilize
each output voltage linearly.
[0031] FIG. 2 illustrates a workflow chart implemented by using a
system of this embodiment, and is used to describe an efficient
control method for a brushless motor with a wide working range
implemented based on the above system. When the system is
initialized, a throttle signal input to the ESC is zero, and the
second DC-DC circuit is simultaneously controlled to output with a
reference voltage. In this way, the ESC executes a self-checking
program.
[0032] The airborne controller receives, through a communication
link, an original throttle signal output by a flight control
system, and the original throttle signal is mapped to the power
demand of the power system so as to obtain a power demand of the
power system at the current time point; and the power demand of the
power system is determined: [0033] when the power demand is less
than or equal to a preset power threshold, the airborne control
system outputs a control signal of the ESC to change an actual
throttle value, and simultaneously controls a second DC-DC circuit
to energize with a reference voltage; and [0034] when the power
demand is greater than the preset power threshold, the airborne
control system simultaneously changes throttle thrust of the ESC
and the output voltage of the second DC-DC circuit according to a
joint adjustment strategy, so as to realize the high-power power
output.
[0035] In a particular embodiment, the power threshold is set at 30
W, and its physical meaning is that when the required power demand
of the system is less than or equal to 30 W, a method for
regulating the throttle by constant-voltage is adopted, and when an
actual power demand is greater than 30 W, the joint adjustment
strategy is adopted to jointly adjust and control both the
operating voltage and ESC input.
[0036] The power threshold is a value input in advance, which is
used to determine whether to transform the voltage of the second
DC-DC circuit, and is generally set at 15% of maximum continuous
operating power of the power system. The reference voltage is the
lowest voltage actually output by the second DC-DC circuit, which
is determined by the lowest voltage supported by the ESC, and may
be the lowest voltage required by the ESC. In a particular
embodiment, the ESC supports input of 3S-6S lithium batteries, and
accordingly, the reference voltage is set at the lowest operating
voltage of 3S lithium batteries, that is 11.1 V.
[0037] The joint adjustment strategy may be implemented by
consulting a known power matching table, so as to correspondingly
output the throttle thrust of the ESC and the output voltage of the
second DC-DC circuit, or alternatively, it may be implemented by a
dynamic tracking algorithm with the objective of tracking the
highest real-time efficiency of the power system by additionally
mounting a corresponding force sensor on a power system.
[0038] The above power matching table records an operating voltage
and throttle thrust of the ESC corresponding to the optimal
efficiency of the system under different power demands. An
efficiency curve of a power device with equal power output under a
target working condition may be obtained in advance through a wind
tunnel test, the operating voltage and throttle thrust
corresponding to the highest efficiency point on the curve as well
as the power are recorded one by one, and efficiency curves of
different equal power outputs may be processed in the same way,
such that the power matching table may be obtained.
[0039] A creation flow of the power matching table is described
below in detail with reference to an efficiency diagram of the
equal power output system in FIG. 3.
[0040] A power test frame is used to constantly adjust an input
voltage of the power system and the throttle thrust of the ESC to
guarantee equal power output. In a particular embodiment, as shown
in the efficiency diagram in FIG. 3, the power system always
maintains equal power output of 60 W, so as to obtain the
efficiency diagram of the power system at different operating
voltages. In FIG. 3, the operating voltage of the system changes
from 10.5 V to 24 V. Although output power remains unchanged, it
may be seen that a maximum efficiency point of the power system
appears when the operating voltage is 12.2 V, and efficiency of the
system exceeds 80%. Then, it may be recorded: when the system is
operated with equal power output 60 W, an optimal operating voltage
should be 12.2 V, and the efficiency of the system at this time
point is 80.5%. By repeating such process, the respective optimal
operating voltages under different working conditions and different
power output of the power system may be acquired, and then the
above power matching table can be obtained.
[0041] The dynamic tracking algorithm may be found from relevant
contents in CN 108791819A in which a dynamic tension detection
device and detection method suitable for an unmanned aerial vehicle
are disclosed, an optimal efficiency value of a tracking system is
achieved through automatic pitch variation, which essentially
tracks an optimal propeller efficiency value of the whole power
system, that is, how much dynamic tension may be brought by power
output per watt. The same idea may be used for establishment of the
dynamic tracking algorithm of the present disclosure. Since the
power system constantly changes the operating voltage and throttle
output and guarantees the output power to be substantially stable,
real-time dynamic tension detected by the dynamic tension detection
device may also be different due to efficiency differences of the
power system under different operating voltages, and a function of
dynamically tracking the highest efficiency of the system may be
achieved by constantly approaching a maximum value of the real-time
tension at a same power.
[0042] In a particular embodiment, mapping the original throttle
signal to the power demand of the power system may directly use
linear mapping. As an example, 0-100% of the original throttle
signal is linearly mapped to a power interval of 0-200 W, that is,
0% of the original throttle signal corresponds to the power demand
of 0 W, 30% of the throttle signal corresponds to the power demand
of 60 W, 60% of the original throttle signal corresponds to the
power demand of 120 W, and 100% of the original throttle signal
corresponds to the power demand of 200 W.
[0043] The control system and method of the present disclosure may
guarantee that the ESC may always operate at an optimal operating
voltage point (instead of only operating in an optimal operating
voltage interval), such that the whole power system is able to
maintain efficient power output in the wide working range.
* * * * *