CN108447338A - IPT flight simulation system with motion system - Google Patents
IPT flight simulation system with motion system Download PDFInfo
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- CN108447338A CN108447338A CN201810386353.8A CN201810386353A CN108447338A CN 108447338 A CN108447338 A CN 108447338A CN 201810386353 A CN201810386353 A CN 201810386353A CN 108447338 A CN108447338 A CN 108447338A
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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
- G09B9/12—Motion systems for aircraft simulators
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- Aviation & Aerospace Engineering (AREA)
- Business, Economics & Management (AREA)
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Abstract
The invention relates to an IPT flight simulation system with a motion system, which is technically characterized in that: the IPT aircraft simulator comprises a base, a fixed platform, a moving platform, an IPT aircraft simulator, a moving system and a moving system cabinet; the IPT aircraft simulator is characterized in that a fixed platform and a moving system are fixedly mounted on the base respectively, the upper portion of the fixed platform is hinged with the front end of the moving platform, the bottom of the rear end of the moving platform is fixedly mounted above the moving system, an IPT aircraft simulator is fixedly mounted above the moving platform, and the IPT aircraft simulator is connected with the moving system through a moving system cabinet and used for controlling the moving system to do telescopic movement along the vertical direction. The teaching quality and the subjective feeling and feedback of the trainees in the learning and training process can be effectively improved, so that the learning quality and the retraining quality are further enhanced.
Description
Technical field
The invention belongs to flight simulator technical fields, are related to the kinematic system of IPT flight simulators, especially a kind of band
There are the IPT flight simulation systems of kinematic system.
Background technology
In recent years, as country supports aircraft industry energetically, science and technology of aviation is also with fast development, various aircrafts and aviation
Equipment is largely provided to grass-roots unit.The thing followed needs to be to have certain economic, efficient mode to carry out being familiar with for equipment,
It trains, the research of rehearsal and related system.With the proposition of these demands, the development of user's also pay attention to day by day training emulator
With development.But it is influenced by the component for the high technology content that equipment itself includes and its complex combination, real plane simulation
The price of device remains high always, not being general training center can bear, and affects various home-built aircrafts at home
Sale and training.And the IPT (Integrated Procedure Trainer) of current prevalence on the market, as shown in Figure 1,
Generally by components such as the top control panels, instrument board, console of polylith touch screen simulator cockpit, provide and actual airplane phase
Close three-dimensional space layout and ratio.The common components such as hood, Mult1purpose Coutrols ＆ Display Unit (MCDU), throttle lever can be used
Part is emulated with training for promotion effect.Student can complete a series of normal procedures and improper/emergence program operation on IPT,
Auxiliary screen provides tenet of dynamic state figure function, is equipped with instructor console's system.
A large amount of fund will be saved by being trained system using IPT, improve the safety of training quality and flight；Make simultaneously
It must train and not limited by objective condition such as weather, places, ensure that the training time, improve training achievement.(note：Due to current
Regulation IPT grades of training aids of civil aviation authority does not have in refreshment and pilot time number, can only be used to flight of imparting knowledge to students and learn by oneself), but it is existing
Some IPT itself cause to substantially reduce flight subjective feeling and practice due to not having kinematic system, so IPT class patterns
Quasi- device cannot be satisfied the refreshment and training of live flying person to for imparting knowledge to students and interest exploitation.
Through retrieval, do not find and the same or analogous patent document having disclosed of the present invention.
Invention content
It is an object of the invention to overcome the deficiencies of the prior art and provide a kind of reasonable design, manufacturing cost it is low and can
Increase the IPT flight simulation systems with kinematic system of subjective sensation of the student during using IPT.
The present invention solves its technical problem and following technical scheme is taken to realize：
A kind of IPT flight simulation systems with kinematic system, including pedestal, fixed platform, motion platform, IPT aircrafts
Simulator, kinematic system and kinematic system cabinet；It is fixed with fixed platform and kinematic system respectively on the pedestal, it is described solid
It being fitted together with the front end of motion platform hinge above fixed platform, the rear end bottom of the motion platform is packed in above kinematic system,
IPT Aircraft Simulators are fixed with above the motion platform, which passes through kinematic system cabinet and kinetic system
System is connected, and vertically makees stretching motion for controlled motion system.
Moreover, the kinematic system is vertically to make the electric actuating cylinder of stretching motion, including rack and electronic work
Dynamic cylinder driving circuit, the rack are hollow cylindrical configuration, are rotated coaxially in bottom of the frame and are connected with axis, on axis successively
Coaxial sleeve is equipped with encoder, retarder and servo motor；It is fixed with leading screw in the axis front end, coaxial sleeve is equipped on leading screw
The piston rod of hollow tube-shape, the piston rod front end are solidly installed with motion platform bottom；It is equipped in piston rod outside front ends
Limiter.
Moreover, the IPT Aircraft Simulators include control stick and foot rudder, kinematic system computer and HOST computers；Institute
The output end for stating control stick and foot rudder is connected with kinematic system computer, the operation signal for generating control stick and foot rudder
To kinematic system computer, which passes through the interface board card module and kinetic system in kinematic system cabinet for output
Control module in system is connected, and works according to the parameter of setting for controlled motion system；The kinematic system computer also with
HOST computers are connected, for realizing the real-time Communication for Power to kinematic system.
Moreover, the kinematic system cabinet includes interface board, kinematic system playback module, safety control module, logic
Power module and retardance resistive module；The safety control module is connected with interface board, for monitoring kinematic system in real time
Operating status and send out fault message to IPT Aircraft Simulators；The safety control module also with kinematic system playback module phase
Connection is playbacked for controlled motion system；The safety control module is also connected with retardance resistive module, for absorbing kinetic system
The extra electromotive force generated when system playback；The interface board card module is connected with retardance resistive module, at the beginning of kinematic system
Circuit detection when beginningization；The logic power module respectively with interface board, electric actuating cylinder playback module, security control mould
Block is connected with retardance resistive module and powers for it.
Moreover, the electric actuating cylinder driving circuit includes control module and driving power module, control module output
End is connected by driving power module with servo motor, the output current for controlling driving power module and control monitoring electricity
Dynamic pressurized strut parameter information；The output end of the control module is connected with retarder, is used for the motion amplitude of controlled motion platform；
The output end of the retarder is connected with servo motor, for reducing servo motor rotating speed according to the control information of control module；
The output end of the servo motor is connected by encoder with control module, for providing turning for servo motor to control module
Fast movement state information；The output end of the limiter respectively with the safety control module in control module and kinematic system cabinet
It is connected, the initial position message for providing piston rod to control module, and the initial position message of the piston rod is exported
Safety control module to kinematic system cabinet；Safety control module in the kinematic system cabinet is connected with retarder
It connects, is recovered under gravity just for controlling electric actuating cylinder when detecting that electric actuating cylinder is in unsafe condition
Beginning position；The output end of logic power module in the kinematic system cabinet respectively with control module, encoder, limiter and subtract
Fast device is connected and powers for it.
The advantages and positive effects of the present invention are：
1, the present invention proposes a kind of novel based on IPT (the i.e. comprehensive journeys of Integrated Procedure Trainer
Sequence training aids) simple driving simulation system can effectively promote religion by increasing kinematic system on the basis of original IPT
The subjective feeling and feedback of quality and student in study and training process are learned, to further strengthen learning quality and refreshment matter
Amount；In addition, the increase of kinematic system, it is possibility to have effect promotes the competitiveness of brand IPT in the market, in the simulation being growing more intense
In device market and occupy certain status in training industry.
2, the present invention carrys out the generation and change of controlled motion system using flight control system and flight attitude, can increase
Subjective sensation of the student during using IPT；It can be used for meeting low expense training requirement and some science popularization sides of grass-roots unit
The requirement in face.The subjective sensation during drive simulation will be promoted and be restored simultaneously, and then effectively improves training effect
With science popularization demonstrating effect.Can also face beginner's progress flight experience simultaneously can also be pre- in face of live flying person's progress refreshment
It practises.
3, the completely new motor of the invention due to use drives pressurized strut, without fluid pressure line and pipe-line control valve, completely
The case where eliminating hydraulic pressure oil seepage brings great convenience for EMM systems to safeguard.
Description of the drawings
Fig. 1 is the overall structure diagram of the present invention；
Fig. 2 is the mechanical structure schematic diagram of the electric actuating cylinder of the present invention；
Fig. 3 is the circuit block diagram of the present invention.
Specific implementation mode
Inventive embodiments are described in further detail below in conjunction with attached drawing：
A kind of IPT flight simulation systems with kinematic system, as shown in Figure 1, including pedestal 6, fixed platform 7, movement
Platform 4, IPT Aircraft Simulators 1, kinematic system 3 and kinematic system cabinet 5；It is fixed with fixed platform respectively on the pedestal
And kinematic system, the fixed platform top and the front end hinge of motion platform are fitted together, the rear end bottom of the motion platform is solid
Above kinematic system, IPT Aircraft Simulators are fixed with above the motion platform, which passes through fortune
Dynamic system cabinet is connected with kinematic system, vertically makees stretching motion for controlled motion system.
In the present embodiment, the kinematic system is vertically to make the electric actuating cylinder of stretching motion, such as Fig. 2 institutes
Show, including rack and electric actuating cylinder driving circuit, the rack is hollow cylindrical configuration, and connection is rotated coaxially in bottom of the frame
There is axis, encoder 3-1, retarder 3-2 and servo motor 3-3 are sequentially coaxially set on axis；In the axis front end
It is fixed with leading screw 3-6, coaxial sleeve is equipped with the piston rod 3-5 of hollow tube-shape, the piston rod front end and motion platform bottom on leading screw
Portion is solidly installed；Limiter 3-7 is installed in piston rod outside front ends, in the output shaft of servo motor and the junction of axis
Also coaxial sleeve is equipped with bearing 4.
Each component of the present invention is formed and is act as：
(1) IPT Aircraft Simulators are the parts Traditional IP T, are fixed on the moving platform, including operator in Traditional IP T
The input of all operationss part and kinematic system is (i.e.：Control stick and foot rudder)；
(2) motion platform front end is fitted together with fixed platform hinge, the fixation for the dot that moves in a circle as motion platform
Fulcrum 2；
(3) kinematic system is to include electric actuating cylinder driving part, servo motor and piston rod in the electric actuating of one
Cylinder, the upper end is packed in motion platform bottom, and lower end is packed on pedestal, and its input terminal and passes through circuit and kinematic system machine
Cabinet connects, and is the power source of entire kinematic system；
(4) Traditional IP T flight simulators are carried above motion platform, front end is connected by bearing with platform fulcrum, after
End is supported by electric actuating cylinder upper end；
(5) kinematic system cabinet is independently positioned over motion platform side, and output end is connected by circuit and electric actuating cylinder
It connects, internal control circuit includes interface board, safety control module and logic power module etc..
In the present embodiment, the IPT Aircraft Simulators are as shown in figure 3, dotted line representation signal line, solid line represent power supply
Line；Including control stick and foot rudder, kinematic system computer and HOST computers；The output end and movement of the control stick and foot rudder
Component computer is connected, for exporting the operation signal of control stick and the generation of foot rudder to kinematic system computer, the movement
Component computer is connected by the interface board card module in kinematic system cabinet with the control module in kinematic system, for controlling
Kinematic system processed works according to the parameter of setting；The kinematic system computer is also connected with HOST computers, for realizing right
The real-time Communication for Power of kinematic system.
Each component of the IPT Aircraft Simulators of the present invention is formed and is act as：
(1) mechanical movement that driver generates the operation of foot rudder, control stick, by corresponding sensor by the behaviour of generation
Make signal transmission and give kinematic system computer, after being calculated by the analysis of kinematic system computer, corresponding state and instruction are transferred to
HOST computers and interface board.
(2) HOST computers, the operation of the entire IPT systems of integrated management, is the information interchange of IPT systems and kinematic system
Center.It is connect with kinematic system computer by 1394 express networks, realizes the real-time Communication for Power to kinematic system.
(3) kinematic system computer, core control part of the kinematic system computer as entire EMM systems, operation control
System software processed.During motion actuated, the configuration file on kinematic system computer can be loaded by interface board
Control module makes electric actuating cylinder work according to the parameter of setting.
In the present embodiment, the kinematic system cabinet as shown in figure 3, the kinematic system cabinet include interface board,
Electric actuating cylinder playback module, safety control module, logic power module and retardance resistive module；The safety control module with
Interface board is connected, and the operating status for monitoring electric actuating cylinder in real time simultaneously sends out failure letter to kinematic system computer
Breath；The safety control module is also connected with electric actuating cylinder playback module, for controlling electric actuating cylinder playback；This is controlled safely
Molding block is also connected with retardance resistive module, and servo motor generates extra electronic when for absorbing electric actuating cylinder playback
Gesture；The interface board card module is connected with retardance resistive module, circuit detection when for electric actuating cylinder initialization；It is described
Logic power module is connected with interface board, electric actuating cylinder playback module, safety control module and retardance resistive module respectively
It connects and powers for it.
Each component of the kinematic system cabinet of the present invention is formed and is act as：
(1) interface board (IFB), in motion control cabinet, IFB plays a part of signal routing and signal processing.This connects
Oralia card is by logic power module for power supply, including a programmable gate array unit, monitoring circuit and various insurance original papers.It is main
It handles and is output to 24V DC power supplies at the signal of the component of control, the various switches for monitoring electric actuating cylinder, driving part
Signal routing and processing of reason, the signal processing of playback component and kinematic system computer etc..
(2) electric actuating cylinder playback component (RTH), i.e. kinematic system playback component (Return To Home) are to move
When system failure or emergency, ensures that electric actuating cylinder can be safely fully retracted, motion platform is made to playback.Than
Such as in EPO, inner link detects fault condition, is also turned on backup DC power source, is provided by special battery pack
It powers to RTH, RTH begins to turn on dynamic retardance resistance circuit, and the electromotive force that pressurized strut retraction generates in the process is enable to be hindered
Stagnant consumed in circuitry.
(3) safety control module, the major function of the module are the operating statuses of real-time monitoring kinematic system, work as kinetic system
System is when there is unsafe condition, as when acceleration is excessive or position sensor (i.e. limiter) gives a warning, safety control module
Instruction is sent out to interface board, stops current action, and fault message is sent out to kinematic system computer.The module also can simultaneously
The input for receiving playback component realizes motion platform playback by controlling correlation module.
(4) logic power module, the major function of the module are circuit, component, biography to kinematic system modules
Sensor etc. provides DC power supply (such as 24V, 15V).To ensure the logic function normal operation of modules.
(5) blocking resistive module, the function of the module is the extra electromotive force that motor generates when absorbing pressurized strut recycling, with
Ensure kinematic system safety.
In the kinematic system of hydraulic-driven, when there is unusual condition, the various relief valves on fluid pressure line while work
Make, the hydraulic oil in the lower cavity of pressurized strut is imported into return line, analog machine platform safety is made to playback.In EMM systems
In system, similar workpiece is equally existed, electricity after replacing various relief valves, retardance resistance that pressurized strut bounces back by RTH components
The power consumption that machine generates falls.
In the present embodiment, the electric actuating cylinder driving circuit is as shown in figure 3, include control module and driving power mould
Block, which is connected by driving power module with servo motor, for controlling the defeated of driving power module
Go out electric current and control monitoring electric actuating cylinder parameter information；The output end of the control module is connected with retarder, for controlling
The motion amplitude of motion platform provides the simultaneously sense of reality of drive simulating person in the pitch direction；The output end of the retarder with
Servo motor is connected, for reducing servo motor rotating speed according to the control information of control module；The output of the servo motor
End is connected by encoder with control module, the rotary speed movement status information for providing servo motor to control module；Institute
The output end for stating limiter is connected with control module and safety control module respectively, for providing piston rod to control module
Initial position message, and the initial position message of the piston rod is exported to the safety control module in kinematic system cabinet；Institute
It states safety control module with retarder to be connected, for controlling electronic work when detecting that electric actuating cylinder is in unsafe condition
Dynamic cylinder is recovered to initial position under gravity；The safety control module is connected with control module, by security control
Module monitors control module state.The output end of logic power module respectively with control module, encoder, limiter and retarder
It is connected and powers for it.
Driving part, i.e. pressurized strut driving (MOTOR DRIVE) are fixed with outside electric actuating cylinder.Driving part is by two
Module forms：Driving power module and control module.Driving power module is used to the AC power of input being converted into direct current
Source is supplied to the direct current brushless servo motor in pressurized strut；Control module be kinematic system cabinet and electric actuating cylinder direct current without
The interface of brush servo motor, the output current of driving power module and control monitor pressurized strut parameters to major function in order to control
Information.(ElectroMechanical Actuator) is the important composition component of entire EMM systems inside electric actuating cylinder, is driven
The brushless DC servomotor for moving the electric actuating cylinder is directly integrated with electric actuating cylinder.
Each component of the electric actuating cylinder of the present invention is formed and is act as：
(1) for encoder coaxial package inside the electric actuating cylinder on axis, major function is to provide work to control module
The movement state informations such as the position and speed of dynamic cylinder.
(2) retarder is fixed on electric actuating cylinder inner wall, in being controlled by controlling the deceleration disk being fixed on axis
Rotating speed, major function are the control information according to control module, reduce motor speed, change motion state.
(3) servo motor is fixed in electric actuating cylinder on the inner wall of middle and lower part, and major function is that electronic dynamic cylinder is made in driving
Movement is the power source of entire kinematic system.
(4) coaxial bearing is sleeved on the output shaft of servo motor and the junction of axis, plays the role of fixed axis.
(5) piston rod is connected by internal thread with pipe group inside pressurized strut, and outer end is connected with motion platform, is pressurized strut
Extension, support when stretching out and shrink as pressurized strut to motion platform.
(6) leading screw is fixed on axis front end, and it acts as stretching and receipts that the kinetic energy of servo motor is converted into piston rod
Contracting kinetic energy.
(7) limiter is fixed on the outside of piston rod, and effect is the initial position that piston rod is made in monitoring, and by location information
It is transferred to safety control module.
Electric actuating cylinder motion process is：When kinematic system computer generates corresponding movement instruction, output to kinetic system
When cabinet control electric actuating cylinder of uniting moves, servo motor powers on, deceleration disk, the encoder for driving axis and being fixed on axis
And guide screw movement, the positive and negative rotation movement of leading screw make piston rod complete reciprocal contractile motion, reach control fortune by screw-driven
The purpose of the up and down of moving platform.The main function of limiter is whether detection pressurized strut returns to fully retracted position, and to
Safety control module in kinematic system cabinet provides location information.
The present invention the course of work be：
After IPT flight simulators start, kinematic system starts to load, and HOST computers are established logical with kinematic system computer
Letter.Kinematic system computer operating system software, while various configuration files being loaded into relevant hardware, it is kinematic system
Operation prepare.After the completion of load, kinematic system can be activated by the motion control button of cockpit.
After activating kinematic system, when driver operates pedal and operating lever, operation information is transmitted by detection sensor
Kinematic system computer, kinematic system computer is given to be directed to the operation information of driver, corresponding information and instruction are passed to
HOST computers and kinematic system cabinet, then HOST computers movement state information is subjected to logical process, and to IPT other
Part sends command adapted thereto, while movement instruction is sent to kinematic system start part by kinematic system cabinet, and executes corresponding
Athletic performance.When operator operates control stick and pedal, corresponding movement instruction is generated by kinematic system computer, then
By kinematic system cabinet, control electric actuating cylinder executes action.By the contractile motion of electric actuating cylinder, after making motion platform
End lifting reduces, and since kinematic system leading edge locus is constant, finally makes to operate the operator of IPT on motion platform in pitching side
Corresponding kinesthesia is generated upwards, and the action for so just completing an IPT kinematic system executes.
The operation principle of the present invention is that：
EMM (The Electromechanical Motion) kinematic system of the present invention is so far most
Advanced full electric simulation kinematic system, the EMM kinematic systems drive entire cockpit flat using completely new electric actuating cylinder
Platform.
The six-degree-of freedom mathematical model of complete dynamic flight simulator, it sits to simulator is provided at three right angles of space x, y, z
The linear motion degree of freedom (around corresponding to, up and down) in parameter direction and around reference axis rotational freedom (corresponding to bowing
It faces upward, roll, yaw).Six-degree-of freedom mathematical model ensures the validity of crew training；And it is suitable for carrying kinetic system in the present invention
The IPT flight simulation systems of system only provide pitching vibrations simulation, because IPT itself is by the top of polylith touch screen simulator cockpit
The components such as portion's control panel, instrument board, console form, and possess outstanding panel connection and careful design unlike moving analog machine entirely,
Therefore too big rise and fall can influence using and designing for IPT.
The present invention can carry out control input according to the push-and-pull and deflection of control stick to kinematic system computer, when operation is driven
When sailing bar, start is carried out according to several and specified actuator of throw of lever start is driven, when wherein aerial statue is changed, fortune
Dynamic system can be provided in the kinesthesia in pitch orientation, while when the state of ground carries out Takeoff and Landing, carry out
Two are becomed privileged judgement, are felt with reaching pushing away back of the body sense and landing in sense of reality.
The present invention carries out control input when using foot rudder according to the stroke of foot rudder to aspect, is made according to foot rudder stroke
It is dynamic that start is carried out to electric actuator, wherein only embodying at 2 points：It is when pedaling rudder in the air, since wing flap and slat start can produce first
Raw significantly rolling carries out what comes into a driver's embodiment by IPT what comes into a driver's, while actuator embodies corresponding kinesthesia in the pitch direction.Its
It is secondary for ground using foot rudder progress braking action, when will produce the brake feel that more significantly leans forward.The generic operation is in ground rank
Section.
Each circuit module in the present invention is all made of commercially available hardware module, can be real using conventional processing method
It is existing.
It is emphasized that invention the embodiment described is illustrative, without being restrictive, because the invention includes simultaneously
It is not limited to the embodiment described in specific implementation mode, it is every to be obtained according to the technical solution of invention by those skilled in the art
Other embodiment also belongs to the range of invention protection.
Claims (5)
1. a kind of IPT flight simulation systems with kinematic system, it is characterised in that：It is flat including pedestal, fixed platform, movement
Platform, IPT Aircraft Simulators, kinematic system and kinematic system cabinet；It is fixed with fixed platform and movement respectively on the pedestal
System, the fixed platform top and the front end hinge of motion platform are fitted together, and the rear end bottom of the motion platform is packed in fortune
Above dynamic system, IPT Aircraft Simulators are fixed with above the motion platform, which passes through kinematic system
Cabinet is connected with kinematic system, vertically makees stretching motion for controlled motion system.
2. a kind of IPT flight simulation systems with kinematic system according to claim 1, it is characterised in that：The fortune
Dynamic system is vertically to make the electric actuating cylinder of stretching motion, including rack and electric actuating cylinder driving circuit, the machine
Frame is hollow cylindrical configuration, is rotated coaxially in bottom of the frame and is connected with axis, and encoder is sequentially coaxially set on axis, is subtracted
Fast device and servo motor；It is fixed with leading screw in the axis front end, coaxial sleeve is equipped with the piston rod of hollow tube-shape on leading screw, should
Piston rod front end is solidly installed with motion platform bottom；Limiter is installed in piston rod outside front ends.
3. a kind of IPT flight simulation systems with kinematic system according to claim 1 or 2, it is characterised in that：It is described
IPT Aircraft Simulators include control stick and foot rudder, kinematic system computer and HOST computers；The control stick and foot rudder it is defeated
Outlet is connected with kinematic system computer, is calculated for exporting the operation signal of control stick and the generation of foot rudder to kinematic system
Machine, the kinematic system computer are connected by the interface board card module in kinematic system cabinet with the control module in kinematic system
It connects, works according to the parameter of setting for controlled motion system；The kinematic system computer is also connected with HOST computers, uses
In realization to the real-time Communication for Power of kinematic system.
4. a kind of IPT flight simulation systems with kinematic system according to claim 1 or 2, it is characterised in that：It is described
Kinematic system cabinet includes interface board, kinematic system playback module, safety control module, logic power module and retardance resistance
Module；The safety control module is connected with interface board, and the operating status for monitoring kinematic system in real time simultaneously flies to IPT
Machine simulator sends out fault message；The safety control module is also connected with kinematic system playback module, is used for controlled motion system
System playback；The safety control module is also connected with retardance resistive module, and it is extra to be generated when for absorbing kinematic system playback
Electromotive force；The interface board card module is connected with retardance resistive module, circuit detection when for kinematic system initialization；Institute
State logic power module respectively with interface board, electric actuating cylinder playback module, safety control module and retardance resistive module phase
It connects and powers for it.
5. a kind of IPT flight simulation systems with kinematic system according to claim 2, it is characterised in that：The electricity
Dynamic pressurized strut driving circuit includes control module and driving power module, the control module output end by driving power module with
Servo motor is connected, the output current for controlling driving power module and control monitoring electric actuating cylinder parameter information；It should
The output end of control module is connected with retarder, is used for the motion amplitude of controlled motion platform；The output end of the retarder with
Servo motor is connected, for reducing servo motor rotating speed according to the control information of control module；The output of the servo motor
End is connected by encoder with control module, the rotary speed movement status information for providing servo motor to control module；Institute
The output end for stating limiter is connected with the safety control module in control module and kinematic system cabinet respectively, is used for control
Module provides the initial position message of piston rod, and the initial position message of the piston rod is exported to kinematic system cabinet
Safety control module；Safety control module in the kinematic system cabinet is connected with retarder, for detect it is electronic
Electric actuating cylinder is controlled when pressurized strut is in unsafe condition is recovered to initial position under gravity；The kinematic system machine
The output end of logic power module in cabinet is connected with control module, encoder, limiter and retarder and is supplied for it respectively
Electricity.
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110827619A (en) * | 2019-12-17 | 2020-02-21 | 江苏无国界无人机科技有限公司 | System for intelligently correcting flight action of student |
| CN112415979A (en) * | 2020-10-30 | 2021-02-26 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Flight control test system, method, equipment and storage medium |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2002123166A (en) * | 2000-10-16 | 2002-04-26 | Nippon Bta Kk | Flight simulator |
| RU48661U1 (en) * | 2004-12-22 | 2005-10-27 | Закрытое Акционерное Общество "Транзас" | INTEGRATED AIRCRAFT SIMULATOR |
| US20080064013A1 (en) * | 2002-05-07 | 2008-03-13 | Remi Quimper | 3-dimensional apparatus for self-paced integrated procedure training and method of using same |
| CN103136979A (en) * | 2011-11-29 | 2013-06-05 | 中国商用飞机有限责任公司 | Airplane comprehensive procedural training device and throttle lever device |
| CN103273447A (en) * | 2013-06-19 | 2013-09-04 | 吉林大学 | Universal precision numerical control support vertical column |
| CN103886782A (en) * | 2014-04-09 | 2014-06-25 | 陈京波 | 360-degree omni-directional overload flight simulator |
| CN205428282U (en) * | 2015-11-30 | 2016-08-03 | 河南三和航空工业有限公司 | Autogyro simulator |
| CN206076504U (en) * | 2016-08-23 | 2017-04-05 | 成都航天万欣科技有限公司 | A kind of adjusting means with auto-lock function |
| CN107424473A (en) * | 2017-08-14 | 2017-12-01 | 徐舒青 | Single seat moves plane simulation steer entirely |
| CN107909883A (en) * | 2017-11-03 | 2018-04-13 | 中国民用航空飞行学院 | Robinson's R44 helicopter multitask flight training devices |
| CN209388516U (en) * | 2018-04-24 | 2019-09-13 | 中航大（天津）模拟机工程技术有限公司 | Novel IPT flight simulation system with motion system |
-
2018
- 2018-04-24 CN CN201810386353.8A patent/CN108447338B/en active Active
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2002123166A (en) * | 2000-10-16 | 2002-04-26 | Nippon Bta Kk | Flight simulator |
| US20080064013A1 (en) * | 2002-05-07 | 2008-03-13 | Remi Quimper | 3-dimensional apparatus for self-paced integrated procedure training and method of using same |
| RU48661U1 (en) * | 2004-12-22 | 2005-10-27 | Закрытое Акционерное Общество "Транзас" | INTEGRATED AIRCRAFT SIMULATOR |
| CN103136979A (en) * | 2011-11-29 | 2013-06-05 | 中国商用飞机有限责任公司 | Airplane comprehensive procedural training device and throttle lever device |
| CN103273447A (en) * | 2013-06-19 | 2013-09-04 | 吉林大学 | Universal precision numerical control support vertical column |
| CN103886782A (en) * | 2014-04-09 | 2014-06-25 | 陈京波 | 360-degree omni-directional overload flight simulator |
| CN205428282U (en) * | 2015-11-30 | 2016-08-03 | 河南三和航空工业有限公司 | Autogyro simulator |
| CN206076504U (en) * | 2016-08-23 | 2017-04-05 | 成都航天万欣科技有限公司 | A kind of adjusting means with auto-lock function |
| CN107424473A (en) * | 2017-08-14 | 2017-12-01 | 徐舒青 | Single seat moves plane simulation steer entirely |
| CN107909883A (en) * | 2017-11-03 | 2018-04-13 | 中国民用航空飞行学院 | Robinson's R44 helicopter multitask flight training devices |
| CN209388516U (en) * | 2018-04-24 | 2019-09-13 | 中航大（天津）模拟机工程技术有限公司 | Novel IPT flight simulation system with motion system |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110827619A (en) * | 2019-12-17 | 2020-02-21 | 江苏无国界无人机科技有限公司 | System for intelligently correcting flight action of student |
| CN112415979A (en) * | 2020-10-30 | 2021-02-26 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Flight control test system, method, equipment and storage medium |
| CN112415979B (en) * | 2020-10-30 | 2021-11-09 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Flight control test system, method, equipment and storage medium |
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