CN207489292U - Simulate aircraft handling operating system - Google Patents
Simulate aircraft handling operating system Download PDFInfo
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- CN207489292U CN207489292U CN201721051235.9U CN201721051235U CN207489292U CN 207489292 U CN207489292 U CN 207489292U CN 201721051235 U CN201721051235 U CN 201721051235U CN 207489292 U CN207489292 U CN 207489292U
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- transmission shaft
- conveyor
- pitching
- electric machine
- tumbling action
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Abstract
A kind of simulation aircraft handling operating system, including left-hand drive operating system；The left-hand drive operating system includes the left steering wheel being made of the first tumbling action mechanism and the first pitching operating mechanism, the first tumbling action resistance feedback system coupled with the first tumbling action mechanism and the first pitching coupled with the first pitching operating mechanism and operates resistance feedback system.Above-mentioned scheme can improve the driving disk operating system sensation simulation fidelity of flight simulation platform, effectively reappear time of day during aircraft flight.
Description
Technical field
The utility model is related to aircraft technology field, more particularly to a kind of simulation aircraft handling operating system.
Background technology
Large transport airplane is the important indicator for weighing a national overall national strength, in the sustainable development of national economy
Play an increasingly important role, Development Techniques are monopolized all the time by American-European countries, import equipment it is of high cost and
Maintenance process is cumbersome, and fly simulation training platform is a kind of important equipment of ground culture pilot, has higher economy
Benefit.
The key component that disk operating system is fly simulation training platform is driven, performance directly determines the instruction of pilot
Practice quality.
But the driving disk operating system of existing flight simulation platform, there is sensation simulation fidelity is not high, it is difficult to
The problem of time of day during effective reproduction aircraft flight.
Invention content
The technical issues of the utility model embodiment solves is how to improve the driving disk operating system of flight simulation platform
Sensation simulation fidelity effectively reappears time of day during aircraft flight.
To solve the above problems, the utility model embodiment provides a kind of simulation aircraft handling operating system, including a left side
Driver behavior system；
It drives on the left side that the left-hand drive operating system includes being made of the first tumbling action mechanism and the first pitching operating mechanism
Sail disk, with the first tumbling action mechanism coupling the first tumbling action resistance feedback system and with first pitching
The first pitching operation resistance feedback system of operating mechanism coupling；
The first tumbling action resistance feedback system includes the first driving wheel, the first driven wheel, the first conveyor, first
Transmission shaft, first angle sensor, the first motor and the first electric machine controller；The first tumbling action mechanism and described first
Driving wheel couples, and first driving wheel is also coupled with first driven wheel, and first driven wheel is also passed with described first
The coupling of defeated band, the first angle sensor are fixedly installed on first transmission shaft, and with first electric machine controller
Coupling, first electric machine controller are also coupled with first motor；
The first angle sensor is detected in real time suitable for the roll angle to first transmission shaft；
First electric machine controller, suitable for obtaining the roll angle of first transmission shaft in real time, and based on described the
The roll angle of one transmission shaft generates corresponding first motor torque control signal, to control the first motor output corresponding
First torque；
First pitching operation resistance feedback system include the first sleeve, the second conveyor, second driving shaft, second jiao
Spend sensor, the second electric machine controller and the second motor；The first pitching operating mechanism is coupled with first sleeve, described
First sleeve is also coupled with second conveyor, and second conveyor is also driven with first transmission shaft and described second
Axis couples, and the second angle sensor is mounted on the second driving shaft, and is coupled with second electric machine controller, institute
The second electric machine controller is stated to couple with second motor；
The second angle sensor, is detected in real time suitable for the roll angle to the second driving shaft；
First electric machine controller, suitable for obtaining the pitch angle of the second driving shaft in real time, and based on described the
The pitch angle of two transmission shafts generates corresponding second motor torque control signal, to control the second motor output corresponding
Second torque.
Optionally, the simulation aircraft handling operating system further includes right driver behavior system and the mechanism that is connected；Institute
Shu You driver behaviors mechanism is coupled by the mechanism that is connected with the left-hand drive operating mechanism；
The mechanism that is connected operates machine suitable for connecting the right driver behavior mechanism when being closed with the left-hand drive
Structure, so that the left-hand drive operating mechanism links with the right driver behavior mechanism；The right driver behavior is disconnected during disconnection
Connection between mechanism and the left-hand drive operating mechanism.
Optionally, the right driver behavior mechanism, including by the second tumbling action mechanism and the second pitching operating mechanism structure
Into left steering wheel, with the second tumbling action mechanism coupling the second tumbling action resistance feedback system and with it is described
The second pitching operation resistance feedback system of second pitching operating mechanism coupling；
The second tumbling action resistance feedback system includes the second driving wheel, the second driven wheel, third conveyor, third
Transmission shaft；The second tumbling action mechanism and second driving wheel couple, second driving wheel also with described second from
Driving wheel couples, and second driven wheel is also coupled with the third conveyor；
The second pitching operation resistance feedback system includes second sleeve, the 4th conveyor, the 4th transmission shaft；Described
Two pitching operating mechanisms are coupled with the second sleeve, and the second sleeve is also coupled with the 4th conveyor, and the described 4th
Conveyor is also coupled with the third transmission shaft and the 4th transmission shaft respectively.
Optionally, the mechanism that is connected includes first clutch and second clutch；
The first clutch is installed between first transmission shaft and the third transmission shaft, suitable for connecting when being closed
Connect first transmission shaft and the third transmission shaft；It is disconnected during disconnection between first transmission shaft and the third transmission shaft
Connection；
The first clutch is installed between the second driving shaft and the 4th transmission shaft, suitable for connecting when being closed
Connect the second driving shaft and the 4th transmission shaft；It is disconnected during disconnection between the second driving shaft and the 4th transmission shaft
Connection.
Optionally, first electric machine controller and second electric machine controller are same controller.
Optionally, first motor is servo alternating current generator.
Optionally, second motor is servo alternating current generator.
Compared with prior art, the technical solution of the utility model has the following advantages that：
Above-mentioned scheme, in driver using the first tumbling action mechanism of left-hand drive operating system to simulating aircraft
When carrying out tumbling action, sensed by the first angle being mounted on the first transmission shaft of the first rolling resistance feedback system
Device detects the roll angle of first transmission shaft in real time, and using described in first electric machine controller in real time acquisition
The roll angle of first transmission shaft, so as to which the roll angle based on first transmission shaft generates corresponding first motor torque control
Signal processed first motor to be controlled to export corresponding first torque-feedback to driver, can so that pilot is real-time
Experience the force feedback from the first rotation mechanism for wind, the power sense of enhancing rolling operation；In driver using left-hand drive operating system
When first pitching operating mechanism carries out pitching operation to simulation aircraft, by being mounted on the first pitching resistance feedback system
The second angle sensor on second driving shaft detects, and use the pitch angle of the second driving shaft in real time
Second electric machine controller obtains the pitch angle of the second driving shaft in real time, so as to bowing based on the second driving shaft
Elevation angle degree generates corresponding second motor torque control signal, second motor to be controlled to export corresponding second torque-feedback
To driver, pilot can be caused to experience the force feedback from the first pitching operating mechanism, enhancing pitching operation in real time
Power sense；It is thus possible to improve the driving disk operating system sensation simulation fidelity of flight simulation platform, effectively reappears aircraft and flies
Time of day during row.
Description of the drawings
Fig. 1 and Fig. 2 is a kind of structure diagram of simulation aircraft handling system in the utility model embodiment；
Fig. 3 is the top cross-sectional view of Fig. 1 and simulation aircraft handling system shown in Fig. 2.
Specific embodiment
To solve the above-mentioned problems in the prior art, the technical solution that the utility model embodiment uses is by driving
When the person of sailing carries out tumbling action using the first tumbling action mechanism of left-hand drive operating system to simulation aircraft, pass through installation
Rolling of the first angle sensor to first transmission shaft on the first transmission shaft of the first rolling resistance feedback system
Gyration is detected in real time, and obtains the roll angle of first transmission shaft in real time using first electric machine controller,
So as to which the roll angle based on first transmission shaft generates corresponding first motor torque control signal, to control described first
Motor exports corresponding first torque-feedback to driver, can pilot is experienced in real time from the first rotation mechanism for wind
Force feedback, enhancing rolling operation power sense；In driver using the first pitching operating mechanism of left-hand drive operating system to simulation
Aircraft carry out pitching operation when, by be mounted on the second driving shaft of the first pitching resistance feedback system described second
Angular transducer detects the pitch angle of the second driving shaft in real time, and real-time using second electric machine controller
The pitch angle of the second driving shaft is obtained, so as to corresponding second electricity of pitch angle generation based on the second driving shaft
Machine Torque Control signal second motor to be controlled to export corresponding second torque-feedback to driver, can to fly
Office staff experiences the force feedback from the first pitching operating mechanism, the power sense of enhancing pitching operation in real time；It is thus possible to improve fly
The driving disk operating system sensation simulation fidelity of row analog platform effectively reappears time of day during aircraft flight.
It is understandable for the above-mentioned purpose of the utility model, feature and advantage is enable to become apparent, below in conjunction with the accompanying drawings to this
The specific embodiment of utility model is described in detail.
Fig. 1 to Fig. 3 respectively illustrates a kind of structure of simulation aircraft handling operating system in the utility model embodiment
Schematic diagram.Refer to Fig. 1 to Fig. 3, a kind of simulation aircraft handling operating system in the utility model embodiment can include a left side
Driver behavior system 1.Left-hand drive operating system 1 is included by the first tumbling action mechanism (not shown) and the first pitching operating mechanism
The left steering wheel 11 and the first tumbling action resistance feedback system of the first tumbling action mechanism coupling that (not shown) is formed, with
And operate resistance feedback system with the first pitching of the first pitching operating mechanism coupling.
Wherein, the first tumbling action resistance feedback system includes the first driving wheel 121, the first driven wheel 122, first transmits
Band 123, the first transmission shaft 124, first angle sensor 125, the first motor 126 and the first electric machine controller (not shown).Its
In, the first tumbling action mechanism is coupled with the first driving wheel 121, and the first driving wheel 121 is also coupled with the first driven wheel 122, the
One driven wheel 122 is also coupled with the first conveyor 123, and first angle sensor 125 is fixedly installed on the first transmission shaft 124,
And coupled with the first electric machine controller, the first electric machine controller is also coupled with the first motor 126.
First pitching operation resistance feedback system include the first sleeve 131, the second conveyor 132, second driving shaft 133,
Second angle sensor 134, the second electric machine controller (not shown) and the second motor 135.Wherein, the first pitching operating mechanism with
First sleeve 131 couples, and the first sleeve 131 is also coupled with the second conveyor 132, and the second conveyor 132 is also passed with first respectively
Moving axis 134 and second driving shaft 133 couple, second angle sensor 134 be mounted on second driving shaft 133 on, and with second electricity
Machine controller couples, and the second electric machine controller is coupled with the second motor 135.
In specific implementation, simulation aircraft handling operating system further includes right driver behavior system 2 and the mechanism that is connected
3.Wherein, right driver behavior mechanism 2 is coupled by the mechanism 3 that is connected with left-hand drive operating mechanism 1.
The mechanism that is connected 2, suitable for connecting right driver behavior mechanism and left-hand drive operating mechanism when being closed, so that a left side is driven
Operating mechanism is sailed to link with right driver behavior mechanism；It is disconnected during disconnection between right driver behavior mechanism and left-hand drive operating mechanism
Connection.
In one embodiment of the utility model, right driver behavior mechanism 2 is included by the second tumbling action mechanism (not shown)
The left steering wheel 21 formed with the second pitching operating mechanism (not shown), the second rolling behaviour coupled with the second tumbling action mechanism
The second pitching made resistance feedback system and coupled with the second pitching operating mechanism operates resistance feedback system.
Second tumbling action resistance feedback system includes the second driving wheel 221, the second driven wheel 222, third conveyor 223
With third transmission shaft 224.Wherein, the second tumbling action mechanism is coupled with the second driving wheel 211, and the second driving wheel 221 is also with
Two driven wheels 222 couple, and the second driven wheel 232 is also coupled with third conveyor 223, and third conveyor 223 is also driven with third
Axis 224 couples.
Second pitching operation resistance feedback system includes second sleeve 231, the 4th conveyor 232 and the 4th transmission shaft 233.
Wherein, the second pitching operating mechanism is coupled with second sleeve 231, and second sleeve 231 is also coupled with the 4th conveyor 232, and the 4th
Conveyor 232 is also coupled with 224 and the 4th transmission shaft 233 of third transmission shaft respectively.
In one embodiment of the utility model, the mechanism that is connected 3 includes first clutch 31 and second clutch 32.Its
In, first clutch 31 is installed between the first transmission shaft 124 and third transmission shaft 224, suitable for the first biography of connection when being closed
Moving axis and third transmission shaft 224；The connection between the first transmission shaft 124 and third transmission shaft 224 is disconnected during disconnection.
First clutch 32 is installed between 134 and the 4th transmission shaft 233 of second driving shaft, suitable for connecting the when being closed
Two transmission shafts and the 4th transmission shaft 233；The connection between 134 and the 4th transmission shaft 233 of second driving shaft is disconnected during disconnection.
The operation principle of above-mentioned simulation aircraft handling operating system will be described in detail below.
When driver pulls 11 left-right rotation of left steering wheel, the first tumbling action in the left steering wheel 11 of left-right rotation
Mechanism drives the first driving wheel 121 to rotate, and the first driving gear 121 drives the first driven wheel 122 to rotate, the first driven wheel 122
The first conveyor 123 is driven to rotate during rotation, the first conveyor 123 drives the first transmission shaft 124 to rotate when rotating.First angle
Sensor 125 detects the rolling rotational angle signal of the first transmission shaft 124, and the rolling that will detect the first transmission shaft 124
Rotational angle signal is delivered separately to plane simulation apparatus control system and the first electric machine controller, plane simulation device control system
It unites and adjusts the roll angle of simulation aircraft nacelle in real time according to angle signal.Meanwhile first electric machine controller detect the first biography
The rolling rotational angle signal of moving axis 124 exports corresponding first motor torque in real time, and pilot is made to be experienced in real time from
The force feedback of one rotation mechanism for wind enhances the power sense of tumbling action.
When rotation before and after driver pulls left steering wheel 11, the first pitching operating mechanism of control wheel 11 moves forward and backward band
Dynamic first sleeve 131 rotates, and the first sleeve 131 drives the second conveyor 132 to rotate while rotation, 132 band of the second conveyor
Dynamic second driving shaft 134 rotates.Second angle sensor 135 detects the pitch rotation angle signal of second driving shaft 134, and
The pitch rotation angle signal for detecting second driving shaft 134 is delivered separately to plane simulation apparatus control system and motor control
Device processed.Plane simulation apparatus control system adjusts mould in real time based on the pitch rotation angle signal for detecting second driving shaft 134
Intend the pitch angle of aircraft nacelle.Meanwhile second electric machine controller according to the pitch rotation angle for detecting second driving shaft 134
Signal generates corresponding second motor torque control signal, the second motor 135 to be controlled to export corresponding second torque in real time, makes
Pilot experiences the force feedback from the first luffing mechanism in real time, enhances pitching operating force sense.
When two drivers manipulate left steering wheel 11 simultaneously and right steering wheel 21 carries out left-right rotation, the first clutch at this time
Device 31 and second clutch 32 are in closed state, and the first transmission shaft 124 and third transmission shaft 224 connect, second driving shaft
133 and the 4th transmission shaft 233 connect, left steering wheel 11 and right steering wheel 21 have identical motion state.11 He of left steering wheel
Right steering wheel 21 left-right rotation and drive link into an integrated entity simultaneously the first transmission shaft 124 and third transmission shaft 224 rotate, and first
Angular transducer 125 detects the rotation of the first transmission shaft 124 and angle signal is transferred to by the first electric machine controller
One motor 126, the first motor 126 is according to the angle signal adjustment rotation received so as to fulfill the flip-flop movement of aircraft.
When two drivers manipulate left steering wheel 11 simultaneously and right steering wheel 21 carries out front and rear rotation, the first clutch at this time
Device 31 and second clutch 32 are in closed state, and the first transmission shaft 124 and third transmission shaft 224 connect, second driving shaft
133 and the 4th transmission shaft 233 connect, left steering wheel 11 and right steering wheel 21 have identical motion state.As two drivers
When manipulating the front and rear rotation of left steering wheel 11 and right steering wheel 21 simultaneously, left steering wheel 11 and the front and rear rotation simultaneously of right steering wheel 21 are simultaneously
The first conveyor 123 and third conveyor 223 is driven to rotate respectively, the first conveyor 123 and third conveyor 223 rotate same
When 133 and the 4th transmission shaft 233 of second driving shaft that links into an integrated entity is driven to rotate, second angle sensor 134 detects the
Four transmission shafts 233 rotate and angle signal are passed to the second motor 135, and the second motor 135 is according to the angle signal received
Adjustment rotates the pitching movement so as to fulfill aircraft.
Using the said program in the utility model embodiment, the first rolling of left-hand drive operating system is used in driver
When operating mechanism carries out tumbling action to simulation aircraft, by the first transmission for being mounted on the first rolling resistance feedback system
The first angle sensor on axis detects the roll angle of first transmission shaft in real time, and uses described first
Electric machine controller obtains the roll angle of first transmission shaft in real time, so as to the roll angle life based on first transmission shaft
Into corresponding first motor torque control signal, first motor to be controlled to export corresponding first torque-feedback to driving
Member can cause pilot to experience the force feedback from the first rotation mechanism for wind, the power sense of enhancing rolling operation in real time；It is driving
When member carries out pitching operation using the first pitching operating mechanism of left-hand drive operating system to simulation aircraft, by being mounted on
Pitching of the second angle sensor to the second driving shaft on the second driving shaft of first pitching resistance feedback system
Angle is detected in real time, and obtains the pitch angle of the second driving shaft in real time using second electric machine controller, from
And the pitch angle based on the second driving shaft generates corresponding second motor torque control signal, to control second electricity
Machine exports corresponding second torque-feedback to driver, can cause pilot experiences in real time to operate machine from the first pitching
The force feedback of structure, the power sense of enhancing pitching operation；It is thus possible to improve the driving disk operating system innervation mould of flight simulation platform
Intend fidelity, effectively reappear time of day during aircraft flight.
The method and system of the utility model embodiment are had been described in detail above, the utility model is not limited to
This.Any those skilled in the art without departing from the spirit and scope of the utility model, can make various changes or modifications,
Therefore the scope of protection of the utility model should be subject to claim limited range.
Claims (7)
1. a kind of simulation aircraft handling operating system, which is characterized in that including left-hand drive operating system；
The left-hand drive operating system include the left steering wheel being made of the first tumbling action mechanism and the first pitching operating mechanism,
With the first tumbling action mechanism coupling the first tumbling action resistance feedback system and with first pitching operate machine
The first pitching operation resistance feedback system of structure coupling；
The first tumbling action resistance feedback system includes the first driving wheel, the first driven wheel, the first conveyor, the first transmission
Axis, first angle sensor, the first motor and the first electric machine controller；The first tumbling action mechanism and the described first active
Wheel coupling, first driving wheel also with first driven wheel couple, first driven wheel also with first conveyor
Coupling, the first angle sensor are fixedly installed on first transmission shaft, and are coupled with first electric machine controller,
First electric machine controller is also coupled with first motor；
The first angle sensor is detected in real time suitable for the roll angle to first transmission shaft；
First electric machine controller suitable for obtaining the roll angle of first transmission shaft in real time, and is passed based on described first
The roll angle of moving axis generates corresponding first motor torque control signal, to control the first motor output corresponding first
Torque；
The first pitching operation resistance feedback system includes the first sleeve, the second conveyor, second driving shaft, second angle and passes
Sensor, the second electric machine controller and the second motor；The first pitching operating mechanism is coupled with first sleeve, and described first
Sleeve is also coupled with second conveyor, and second conveyor is also driven with first transmission shaft and described second respectively
Axis couples, and the second angle sensor is mounted on the second driving shaft, and is coupled with second electric machine controller, institute
The second electric machine controller is stated to couple with second motor；
The second angle sensor, is detected in real time suitable for the roll angle to the second driving shaft；
First electric machine controller suitable for obtaining the pitch angle of the second driving shaft in real time, and is passed based on described second
The pitch angle of moving axis generates corresponding second motor torque control signal, to control the second motor output corresponding second
Torque.
2. simulation aircraft handling operating system according to claim 1, which is characterized in that further include right driver behavior system
With the mechanism that is connected；The right driver behavior mechanism passes through mechanism and the left-hand drive operating mechanism coupling of being connected
It connects；
The mechanism that is connected, suitable for connecting the right driver behavior mechanism and the left-hand drive operating mechanism when being closed, with
So that the left-hand drive operating mechanism links with the right driver behavior mechanism；Disconnected during disconnection the right driver behavior mechanism with
Connection between the left-hand drive operating mechanism.
3. simulation aircraft handling operating system according to claim 2, which is characterized in that the right driver behavior mechanism,
Including the left steering wheel being made of the second tumbling action mechanism and the second pitching operating mechanism and the second tumbling action mechanism
Second tumbling action resistance feedback system of coupling and the second pitching operation resistance with the second pitching operating mechanism coupling
Force feedback system；
The second tumbling action resistance feedback system includes the second driving wheel, the second driven wheel, third conveyor and third and passes
Moving axis；The second tumbling action mechanism is coupled with second driving wheel, and second driving wheel is also driven with described second
Wheel coupling, second driven wheel also with the third conveyor couple, the third conveyor also with the third transmission shaft
Coupling；
The second pitching operation resistance feedback system includes second sleeve, the 4th conveyor, the 4th transmission shaft；
The second pitching operating mechanism and the second sleeve couple, the second sleeve also with the 4th conveyor coupling
It connects, the 4th conveyor is also coupled with the third transmission shaft and the 4th transmission shaft respectively.
4. simulation aircraft handling operating system according to claim 3, which is characterized in that the mechanism that is connected includes
First clutch and second clutch；
The first clutch is installed between first transmission shaft and the third transmission shaft, suitable for connecting institute when being closed
State the first transmission shaft and the third transmission shaft；The company between first transmission shaft and the third transmission shaft is disconnected during disconnection
It connects；
The first clutch is installed between the second driving shaft and the 4th transmission shaft, suitable for connecting institute when being closed
State second driving shaft and the 4th transmission shaft；The company between the second driving shaft and the 4th transmission shaft is disconnected during disconnection
It connects.
5. it is according to claim 1 simulation aircraft handling operating system, which is characterized in that first electric machine controller and
Second electric machine controller is same controller.
6. simulation aircraft handling operating system according to claim 1, which is characterized in that first motor is handed over for servo
Galvanic electricity machine.
7. simulation aircraft handling operating system according to claim 1, which is characterized in that second motor is handed over for servo
Galvanic electricity machine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721051235.9U CN207489292U (en) | 2017-08-22 | 2017-08-22 | Simulate aircraft handling operating system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721051235.9U CN207489292U (en) | 2017-08-22 | 2017-08-22 | Simulate aircraft handling operating system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207489292U true CN207489292U (en) | 2018-06-12 |
Family
ID=62485100
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721051235.9U Active CN207489292U (en) | 2017-08-22 | 2017-08-22 | Simulate aircraft handling operating system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207489292U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107316533A (en) * | 2017-08-22 | 2017-11-03 | 中仿智能科技（上海）股份有限公司 | Simulate aircraft handling operating system |
| CN111547263A (en) * | 2020-05-09 | 2020-08-18 | 陕西飞机工业（集团）有限公司 | Method for testing ground dynamic characteristics of airplane control system |
-
2017
- 2017-08-22 CN CN201721051235.9U patent/CN207489292U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107316533A (en) * | 2017-08-22 | 2017-11-03 | 中仿智能科技（上海）股份有限公司 | Simulate aircraft handling operating system |
| CN107316533B (en) * | 2017-08-22 | 2023-08-15 | 中仿智能科技（上海）股份有限公司 | Simulated aircraft pilot operating system |
| CN111547263A (en) * | 2020-05-09 | 2020-08-18 | 陕西飞机工业（集团）有限公司 | Method for testing ground dynamic characteristics of airplane control system |
| CN111547263B (en) * | 2020-05-09 | 2023-03-14 | 陕西飞机工业（集团）有限公司 | Method for testing ground dynamic characteristics of airplane control system |
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