CN109461345A - A kind of seat system that pilot can be made to have overload to experience when driving flight simulator - Google Patents
A kind of seat system that pilot can be made to have overload to experience when driving flight simulator Download PDFInfo
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- CN109461345A CN109461345A CN201811402253.6A CN201811402253A CN109461345A CN 109461345 A CN109461345 A CN 109461345A CN 201811402253 A CN201811402253 A CN 201811402253A CN 109461345 A CN109461345 A CN 109461345A
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
- G09B9/10—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer with simulated flight- or engine-generated force being applied to aircraft occupant
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Abstract
The present invention relates to flight-simulation equipment technical fields, and disclose a kind of seat system that pilot can be made to have overload to experience when driving flight simulator, including hardware device and software, the hardware device includes motion control cabinet and overload seat, overload seat industrial control computer is installed in the control cabinet, four motor drivers and system power supply, motion control card is installed in the overload seat industrial control computer, the overload seat software that the dynamic data of processing flight simulator is received and analyzed by Ethernet is installed in the overload seat industrial control computer, the overload seat includes chair body and bracket.The seat system can make pilot have preferable overload impression.
Description
Technical field
The present invention relates to flight-simulation equipment technical fields, specially a kind of that pilot can be made to drive flight simulator
When have overload experience seat system.
Background technique
Flight simulator has various configurations, one of them very big difference is exactly that whether there is or not six-degree-of freedom mathematical model, movements
System can be provided for pilot longitudinal direction (front and back), laterally (left and right), the sensation of acceleration on vertical (upper and lower) three directions with
And the angular acceleration around these three directions feels (six degree of freedom), makes entire flight simulation process more close to true, but makes
With the flight simulator cost of kinematic system is high, occupied area is huge, installation limitation is more, working service is at high cost, safety is wanted
Ask more, the flight simulator without kinematic system can not provide kinaesthesis for pilot again or overload is felt, pilot
In-flight feel untrue.
The most kinematic system in current domestic market is all object game, and small-sized kinematic system has fraction big
Type kinematic system product, also because the development time of this technology is not long and complicated in the presence of debugging, consuming time is long, movement effect
The problems such as fruit is poor, maintainability is poor, high failure rate, therefore it is mostly used in the flight simulator of pilot training, all directly from state
Outer import matured product, and external kinematic system is substantially all in the price of millions of members, along with the flight with kinematic system
Simulator require require to all hardware equipment thereon will Fine design, as projector must use can go up motion platform
Projector, get off in this way, the price of flight simulator entirety is than without the much higher of kinematic system, it could even be possible to turning over
Times.
It is overload seat there are also a kind of lower-cost equipment that can provide kinaesthesis for pilot, can provides
Sensation of acceleration on longitudinal (front and back), laterally (left and right), vertical (upper and lower) three directions, but can not provide around these three
The angular acceleration in direction is felt, is mounted in flight simulator at low cost, occupied area is small, debugging cycle is short, maintenance side
Just the advantages that, there is matured product in such as U.S. MOOG company external at present, but embargos to the country, and the country is currently without company
Overload seat is succeeded in developing, closest is to buffet seat, i.e., installs 4 motors, root below the monolithic seat of flight simulator
According to flight simulator real flight conditions, electric machine frequency and amplitude variations make seat generate either large or small shake, only provide
Vertical innervation, take off on this implementation simulation ground or descent in vibrating effect it is preferable, but for flight
In whole process compound dynamic emulation impression and it is bad.
Summary of the invention
(1) the technical issues of solving
In view of the deficiencies of the prior art, it can make pilot when driving flight simulator the present invention provides a kind of
The seat system for having overload to experience, having makes pilot have the advantages that preferably to overload and experience, and solves not no kinematic system
Flight simulator can not provide kinaesthesis for pilot or overload is felt, feel false problem in pilot flight.
(2) technical solution
To realize the purpose for making pilot have preferable overload impression, the invention provides the following technical scheme: a kind of can make
The seat system that pilot has overload to experience when driving flight simulator, including hardware device and software, the hardware
Equipment includes motion control cabinet and overload seat, overload seat industrial control computer is equipped in the control cabinet, four motors drive
Device and system power supply are moved, motion control card is installed in the overload seat industrial control computer, the overload seat industry control calculates
The overload seat software that the dynamic data of processing flight simulator is received and analyzed by Ethernet is installed in machine, overloads seat
The major function of chair software is that the real-time flight parameter for receiving flight simulator by network is converted into four by data processing
The kinematic parameter of a motor calls the api function of motion control card, and four motors is driven to be acted accordingly, gives pilot
Experienced with the overload of all directions, the overload seat includes chair body and bracket, and sliding rail and the first servo are housed on the bracket
The pedestal installation part of motor, the pedestal of the first servo motor are mechanically anchored in chair body, make chair body by telescope motor connecting rod
It can move up and down along sliding rail, with the adjusting seat height function of simulating realistic aircraft, the chair back and cushion of the chair body are set
For movable structure, second servo motor, third servo motor, the 4th servo motor pedestal be mechanically anchored in chair body
On, the link mechanism of second servo motor is mechanically connected to backrest, makes backrest by telescope motor connecting rod
It can move left and right, simulate side caused by the side-friction force when aircraft has side acceleration between human body and aircraft backrest
Sliding to feel, the link mechanism of the third servo motor is mechanically connected to backrest, leans on seat by telescope motor connecting rod
Back can be moved forward and backward, and when simulating aircraft acceleration and deceleration or pitch angle variation, pilot, which experiences, to push away back sense or feel from back, described
The link mechanism of 4th servo motor is mechanically connected to Chain cushion, keeps Chain cushion upward by telescope motor connecting rod
Or move down, simulate under aircraft shafting, pilot experiences vertical positive minusg or when pitch angle changes, buttocks with
Pressure changing between cushion, i.e., overweight or weightless sense, the first servo motor, the second servo motor, third are watched
It takes motor and the 4th servo motor passes through dedicated signal lines and is connected on respective motor driver, four motor drivers
It is connected by cable and is connected to motion control card；
The software includes initialization module and data processing module, and initialization module includes to read driver configuration text
Part module, read season profile module, starting seat motor module, starting timer module, initialization network module and
Initialize interface module, data processing module include network receive flight data module, calculate flight data averaging module,
It calculates flight data change rate module, calculate flap influence module, verify data module and moved seat module, overload seat
Chair software receives by Ethernet and analyzes the dynamic data of processing flight simulator, passes through 4 motors of motion control card control
Driver drives corresponding motor, has seat and adjusts height function, and does the backrest being connected to the motor and cushion
Left and right, front and back, upper and lower compound motion, thus to pilot with the overload impression on front and rear, left and right, upper and lower three directions.
Preferably, the motion control card is installed in the pci card slot of overload seat industrial control computer.
Preferably, the overload seat is specially to emulate fighter plane ejector seat.
Preferably, the concrete model of the motion control card is ZMP-SynqNet-PCI-RJ.
Preferably, the concrete model of the motor driver is AKD-B00606-BNSQ-0000.
(3) beneficial effect
Compared with prior art, pilot can be made to have when driving flight simulator the present invention provides a kind of
Carry impression seat system, have it is following the utility model has the advantages that
1, the seat system that pilot can be made to have overload to experience when driving flight simulator, is watched by first
Take the flexible function of making overload seat realize that height of seat is adjusted along sliding rail up and down motion of link mechanism of motor, the second servo
The link mechanism of motor is mechanically connected to backrest, moves left and right backrest by telescope motor connecting rod, simulation
It breaks away and feels caused by side-friction force when aircraft has side acceleration between human body and aircraft backrest, third servo electricity
The link mechanism of machine is mechanically connected to backrest, is moved forward and backward backrest by telescope motor connecting rod, and simulation flies
Pilot, which experiences, when machine acceleration and deceleration or pitch angle change pushes away back or the feeling from back, the link mechanism machine of the 4th servo motor
Tool is connected to Chain cushion, moves up or down Chain cushion by telescope motor connecting rod, simulates in aircraft axis
Under system, when pilot experiences vertical positive minusg or pitch angle variation, the pressure changing between buttocks and cushion,
I.e. overweight or weightless sense, overload seat software are received and are analyzed by Ethernet the dynamic data of processing flight simulator, passes through
Four motor drivers of motion control card control drive corresponding motor, have seat and adjust height function, and make and motor phase
Backrest and cushion even does left and right, front and back, upper and lower compound motion, to give pilot with front and rear, left and right, three upper and lower
Overload impression on direction.
2, the seat system that pilot can be made to have overload to experience when driving flight simulator, passes through what is be equipped with
Software, software calculate flight parameter related to overload seat all directions motion motor, and it is related to be converted into each motor
Kinematic parameter, driving motor, which moves, gives people's innervation, can be with for the user being limited to when cost, place, maintenance
The degree true to nature that flight simulator is promoted using this system is felt to imply to pilot to overload.
Detailed description of the invention
Fig. 1 is a kind of seat that pilot can be made to have overload to experience when driving flight simulator proposed by the present invention
The software flow pattern of chair system；
Fig. 2 is a kind of seat that pilot can be made to have overload to experience when driving flight simulator proposed by the present invention
The hardware device attachment structure schematic diagram of chair system；
Fig. 3 is a kind of seat system that pilot can be made to have overload to experience when driving flight simulator proposed by the present invention
The function structure schematic diagram of system.
Specific embodiment
The technical solution in the present invention will be clearly and completely described below, it is clear that described embodiment is only
It is only a part of the embodiment of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, the common skill in this field
Art personnel every other embodiment obtained without making creative work belongs to the model that the present invention protects
It encloses.
A kind of seat system that pilot can be made to have overload to experience when driving flight simulator referring to FIG. 1-2,
System, including hardware device and software, hardware device include motion control cabinet and overload seat, are equipped with overload seat in control cabinet
Chair industrial control computer, four motor drivers and system power supply overload in seat industrial control computer and are equipped with motion control card,
The overload that the dynamic data of processing flight simulator is received and analyzed by Ethernet is installed in overload seat industrial control computer
Seat software, the major function of overload seat software is that the real-time flight parameter of flight simulator is received by network, by number
According to processing, it is converted into the kinematic parameter of four motors, calls the api function of motion control card, drives four motors to carry out corresponding
Movement, experienced to pilot with the overloads of all directions, overload seat includes chair body and bracket, on bracket equipped with sliding rail and
The pedestal installation part of first servo motor, the pedestal of first servo motor are mechanically anchored on pedestal installation part, the first servo electricity
It is whole that the link mechanism of machine is mechanically connected to overload seat, and the chair back and cushion for overloading seat are set as movable structure, and described the
Two servo motors, third servo motor, the 4th servo motor pedestal be mechanically anchored in chair, the company of the second servo motor
Linkage is mechanically connected to backrest, moves left and right backrest by telescope motor connecting rod, and simulation has when aircraft
It breaks away and feels caused by frictional force lateral between human body and aircraft backrest when side acceleration, the connecting rod of third servo motor
Mechanism is mechanically connected to backrest, is moved forward and backward backrest by telescope motor connecting rod, simulates aircraft acceleration and deceleration
Or when pitch angle variation, pilot, which experiences, to push away back sense or feels from back, and the link mechanism of the 4th servo motor is mechanically connected to seat
Cushion moves up or down Chain cushion by telescope motor connecting rod, simulates the pilot under aircraft shafting
When experiencing vertical positive minusg or pitch angle variation, the pressure changing between buttocks and cushion is that is, overweight or weightless
Sense, first servo motor, the second servo motor, third servo motor and the 4th servo motor are connected by dedicated signal lines
Onto respective motor driver, four motor drivers are connected by cable and are connected to motion control card；
Software includes initialization module and data processing module, and initialization module includes to read driver configuration file mould
Block reads season profile module, starting seat motor module, starting timer module, initialization network module and initial
Change interface module, data processing module includes that network receives flight data module, calculates flight data averaging module, calculates
Flight data change rate module calculates flap influence module, verify data module and moved seat module, and it is soft to overload seat
Part receives by Ethernet and analyzes the dynamic data of processing flight simulator, passes through 4 motor drivens of motion control card control
Device drives corresponding motor, has seat and adjusts height function, and make the backrest being connected to the motor and cushion do left and right,
Front and back, upper and lower compound motion, thus to pilot with the overload impression on front and rear, left and right, upper and lower three directions.
Motion control card is installed in the pci card slot of overload seat industrial control computer.
Overloading seat is specially to emulate fighter plane ejector seat.
The concrete model of motion control card is ZMP-SynqNet-PCI-RJ.
The concrete model of motor driver is AKD-B00606-BNSQ-0000.
A kind of calculation method of the motor movement parameter based on claim 1-5, includes the following steps:
S1. interior aircraft longitudinal axis direction (X-axis) acceleration of newest 3 execution cycles (30ms), aircraft plate angle are calculated
Degree, aircraft pitch angle, overload values at pilot, aircraft yaw angle average value, be denoted as Avg_Acc_X, Avg_Angle_ respectively
AirBrake,Avg_P,Avg_GLoad,Avg_SideSlip；
It calculates interior aircraft longitudinal axis direction (X-axis) acceleration of newest 3 execution cycles (30ms), aircraft air brake angle, fly
The change rate of overload values at machine pitch angle, pilot, aircraft yaw angle, is denoted as Rate_Acc_X, Rate_Angle_ respectively
AirBrake,Rate_P,Rate_GLoad,Rate_SideSlip；
MotionSurge, MotionSway, MotionSeatPan: being kinematic parameter structural body MotionPara
The kinematic parameter of motor, structural body statement are as follows above and below instance objects, respectively backrest front and back, backrest or so, cushion:
The target movement position calculation formula of corresponding 3 motors is as follows around calculating backrest, above and below cushion:
Calculate target movement position
(1) .MotionSurge.pos=1*Avg_Acc_X-1*sin (π/180.0 Avg_Angle_AirBrake*)+
3*sin(Avg_P*π/180.0)+3*(Avg_GLoad-1)；
In above formula,
■ sin (angle): mathematical function returns to the sine value of angle (radian)；
■ Avg_Acc_X: the average value of aircraft longitudinal axis directional acceleration；
■ Avg_Angle_AirBrake: the angular average of flap；
■ Avg_P: aircraft pitch angle average value；
■ Avg_GLoad: overload values average value at pilot, putting down is 1 when flying；
(2) .MotionSway.pos=Avg_SideSlip；
In above formula,
■ Avg_SideSlip: aircraft yaw angle average value；
(3) (π/180.0 (90-Avg_P) *) .MotionSeatPan.pos=3* (Avg_GLoad-1)-cos；
In above formula,
■ cos (angle): mathematical function returns to the cosine value of angle (radian)；
■ Avg_GLoad: overload values average value at pilot, putting down is 1 when flying；
■ Avg_P: aircraft pitch angle average value；
S2. acceleration of motion, deceleration, maximum target speed are calculated
Because single motion is a time-continuing process, the time is needed to complete, in order to infrequently interrupt last fortune
It is dynamic, the difference of motor target movement position and current location is calculated, it is relevant according to each motor movement if difference > 0.1
Flight parameter calculates the acceleration of this movement, deceleration, shown in following formula:
(4) .MotionSurge.acceleration=25+ (Rate_Acc_X+Rate_Angle_AirBra ke+
Rate_P+Rate_GLoad)/4.0*20；
(5) .MotionSurge.deceleration=25+ (Rate_Acc_X+Rate_Angle_AirBra ke+
Rate_P+Rate_GLoad)/4.0*20；
(6) .MotionSurge.velocity=sqrt ((MotionSurge.acceleration*
MotionSurge.pos)/2)；
(7) .MotionSway.acceleration=25+Rate_SideSlip*20；
(8) .MotionSway.deceleration=25+Rate_SideSlip*20；
(9) .MotionSway.velocity=sqrt ((MotionSway.acceleration*
MotionSway.pos)/2)；
(10) .MotionSeatPan.acceleration=25+ (3* (Avg_GLoad-1)-cos ((90-Avg_P) *
π/180.0))*20；
(11) .MotionSeatPan.deceleration=25+ (3* (Avg_GLoad-1)-cos ((90-Avg_P) *
π/180.0))*20；
(12) .MotionSeatPan.velocity=sqrt ((MotionSeatPan.acceleration *
MotionSeatPan.pos)/2)；
In above formula, sqrt is mathematical function, returns to the square root that sqrt is passed to parameter；
S3. motor target position is verified
Judge the movement velocity V0 with current motor, slows down according to the deceleration of MotionSurge.deceleration
The distance S_dec=V02/2/deceleration passed through to 0 is less than motor target position pos, illustrates target position, adds
This 3 parameters of speed, deceleration are available, otherwise modify motor target position pos=V02/2/deceleration；
S4. motor maximum target speed is verified
Judge that if highest goal speed velocity is less than motor current kinetic speed V0, assigned again to velocity
Value improves target velocity, so that motor is still done trapezoidal motion, assignment is as follows:
(13) .MotionSurge.velocity=V0+ (V0-MotionSurge.velocity)/2.0；
(14) .MotionSway.velocity=V0+ (V0-MotionSway.velocity)/2.0；
(15) .MotionSeatpan.velocity=V0+ (V0-MotionSeatpan.velocity)/2.0；
In above formula,
■ V0: current motor movement velocity；
The parameters of target motion of backrest front and back motor, backrest or so motor, cushion or more motor are calculated above, so
Motor movement function mpiMotionTrapezoidalMove is called afterwards, is passed to relevant parameter, then motor is moved；
S5. motor movement function
Motor movement function prototype and meaning are as follows:
MpiMotionTrapezoidalMove (MPIMotion motion, double position, double
Velocity, double acceleration, double deceleration)；
The incoming function parameter meaning of above-mentioned api function prototype is as described below:
■ MPIMotion motion: motor before and after specified motor movement object, including height of seat motor, backrest leans on
Carry on the back left and right motor, cushion height motor；
■ float position: the target position of specified motor；
■ float velocity: the maximum speed of specified motor；
■ float acceleration: specified motor reaches the acceleration of maximum speed；
■ float deceleration: specified motor reaches the deceleration of target position；
The effect of this function is to make specified motor from stopping one trapezoidal motion of output is started to, that is, assumes currently assigned electricity
Machine connecting rod position is p0, and after calling this function, motor connection lever accelerates to speed with the uniform acceleration of acceleration
Then velocity carries out uniformly retarded motion and rests on the position p1 maintained until acceleration deceleration can be used,
It is as shown in Figure 3:
Note: call mpiMotionTrapezoidalMove function when, incoming parameter include target position, acceleration,
Deceleration, maximum speed, will be multiplied by the corresponding gain coefficient of corresponding motor, and specific value is as follows:
■ height of seat module, gain coefficient value=1690932006.2992
Module before and after ■ backrest, gain coefficient value=1085672288.7111
■ backrest or so module, gain coefficient value=382769076.1481
■ seat support basin module, gain coefficient value=634700722.6311.
In conclusion the seat system, in use, being stretched by the link mechanism of first servo motor makes to overload seat
Move up and down the function of realizing that height of seat is adjusted along sliding rail, and the link mechanism of the second servo motor is mechanically connected to seat and leans on
Back, moves left and right backrest by telescope motor connecting rod, simulation human body and aircraft when aircraft has side acceleration
It breaks away and feels caused by frictional force between backrest, the link mechanism of third servo motor is mechanically connected to backrest, passes through
Telescope motor connecting rod is moved forward and backward backrest, when simulating aircraft acceleration and deceleration, the link mechanism machine of the 4th servo motor
Tool is connected to Chain cushion, moves up or down Chain cushion by telescope motor connecting rod, simulates in aircraft shafting
Under, when pilot experiences vertical positive minusg, pressure changing between buttocks and cushion, i.e., overweight or weightless sense,
Pilot, which experiences, to push away back sense or feels from back, and overload seat software is received by Ethernet and analyzes processing flight simulator
Dynamic data drives corresponding motor by four motor drivers of motion control card control, has seat and adjust height function
Can, and the backrest being connected to the motor and cushion is made to do left and right, front and back, upper and lower compound motion, thus to before pilot
Afterwards, it controls, the overload impression on upper and lower three directions, is progress software development on the basis of specific hardware through the invention,
Including hardware and software, by that will be calculated in overload seat all directions motion motor correlation flight parameter in software,
It is converted into the relevant kinematic parameter of each motor, driving motor, which moves, gives people's innervation, for being limited to cost, place, maintenance etc.
In the case of user, this system can be used to promote the degree true to nature of flight simulator, feels dark to pilot to overload
Show.
It should be noted that the terms "include", "comprise" or its any other variant are intended to the packet of nonexcludability
Contain, so that the process, method, article or equipment for including a series of elements not only includes those elements, but also including
Other elements that are not explicitly listed, or further include for elements inherent to such a process, method, article, or device.
In the absence of more restrictions, the element limited by sentence "including a ...", it is not excluded that including the element
Process, method, article or equipment in there is also other identical elements.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (5)
1. it is a kind of can make pilot have when driving flight simulator overload experience seat system, including hardware device and
Software, it is characterised in that:
The hardware device includes motion control cabinet and overload seat, and overload seat industry control is equipped in the control cabinet and is calculated
Machine, four motor drivers and system power supply are equipped with motion control card, the overload in the overload seat industrial control computer
The overload seat that the dynamic data of processing flight simulator is received and analyzed by Ethernet is installed in seat industrial control computer
Software, the overload seat include chair body and bracket, and the pedestal installation part of sliding rail and first servo motor is housed on the bracket,
The pedestal of the first servo motor is mechanically anchored on pedestal installation part, and the link mechanism of first servo motor is mechanically connected to
Chair body, the chair back and cushion of the chair body are set as movable structure, and second servo motor, third servo motor, the 4th watch
The pedestal for taking motor is mechanically anchored in chair, and the link mechanism of second servo motor is mechanically connected to backrest, institute
The link mechanism for stating third servo motor is mechanically connected to backrest, the link mechanism mechanical connection of the 4th servo motor
To Chain cushion, the first servo motor, the second servo motor, third servo motor and the 4th servo motor pass through dedicated
Signal wire is connected on respective motor driver, and four motor drivers are connected by cable and are connected to motion control card；
The software includes initialization module and data processing module, and initialization module includes to read driver configuration file mould
Block reads season profile module, starting seat motor module, starting timer module, initialization network module and initial
Change interface module, data processing module flies comprising network reception flight data module, calculating flight data averaging module, calculating
Join data variation rate module, calculate flap influence module, verify data module and moved seat module.
2. a kind of seat that pilot can be made to have overload to experience when driving flight simulator according to claim 1
System, it is characterised in that: the motion control card is installed in the pci card slot of overload seat industrial control computer.
3. a kind of seat that pilot can be made to have overload to experience when driving flight simulator according to claim 1
System, it is characterised in that: the overload seat is specially to emulate fighter plane ejector seat.
4. a kind of seat that pilot can be made to have overload to experience when driving flight simulator according to claim 1
System, it is characterised in that: the concrete model of the motion control card is ZMP-SynqNet-PCI-RJ.
5. a kind of seat that pilot can be made to have overload to experience when driving flight simulator according to claim 1
System, it is characterised in that: the concrete model of the motor driver is AKD-B00606-BNSQ-0000.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811402253.6A CN109461345A (en) | 2018-11-23 | 2018-11-23 | A kind of seat system that pilot can be made to have overload to experience when driving flight simulator |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811402253.6A CN109461345A (en) | 2018-11-23 | 2018-11-23 | A kind of seat system that pilot can be made to have overload to experience when driving flight simulator |
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| Publication Number | Publication Date |
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| CN109461345A true CN109461345A (en) | 2019-03-12 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110085088A (en) * | 2019-06-05 | 2019-08-02 | 福州高新区玲富科技有限公司 | A kind of airport baby plane seating simulation detection system |
| CN111803870A (en) * | 2020-07-23 | 2020-10-23 | 中国人民解放军空军军医大学 | Multi-posture vestibular function training platform |
-
2018
- 2018-11-23 CN CN201811402253.6A patent/CN109461345A/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110085088A (en) * | 2019-06-05 | 2019-08-02 | 福州高新区玲富科技有限公司 | A kind of airport baby plane seating simulation detection system |
| CN110085088B (en) * | 2019-06-05 | 2021-01-26 | 南京奔联软件科技有限公司 | Small airplane riding simulation detection system for airport |
| CN111803870A (en) * | 2020-07-23 | 2020-10-23 | 中国人民解放军空军军医大学 | Multi-posture vestibular function training platform |
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Application publication date: 20190312 |