CN112735223A - Flight simulation training device - Google Patents
Flight simulation training device Download PDFInfo
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- CN112735223A CN112735223A CN202011528792.1A CN202011528792A CN112735223A CN 112735223 A CN112735223 A CN 112735223A CN 202011528792 A CN202011528792 A CN 202011528792A CN 112735223 A CN112735223 A CN 112735223A
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- 238000004088 simulation Methods 0.000 title claims abstract description 77
- 238000012549 training Methods 0.000 title claims abstract description 32
- 230000033001 locomotion Effects 0.000 claims description 23
- 239000003638 chemical reducing agent Substances 0.000 claims description 9
- 238000004891 communication Methods 0.000 claims description 6
- 230000009471 action Effects 0.000 abstract description 11
- 230000000694 effects Effects 0.000 abstract description 3
- 241000270295 Serpentes Species 0.000 description 5
- 238000000034 method Methods 0.000 description 5
- 230000008569 process Effects 0.000 description 4
- 239000008358 core component Substances 0.000 description 2
- 230000004438 eyesight Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 241000272060 Elapidae Species 0.000 description 1
- 241000030013 Poga Species 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 210000004556 brain Anatomy 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
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- 208000002173 dizziness Diseases 0.000 description 1
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- 230000006870 function Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000013178 mathematical model Methods 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 230000001720 vestibular Effects 0.000 description 1
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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
- G09B9/16—Ambient or aircraft conditions simulated or indicated by instrument or alarm
- G09B9/20—Simulation or indication of aircraft attitude
- G09B9/206—Simulation or indication of aircraft attitude for in-flight condition
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Abstract
The invention relates to a driving simulation device, in particular to a flight simulation training device, which comprises: the device comprises a portal frame fixed on the ground, a transverse moving device fixed on the portal frame, a vertical moving device fixed on the transverse sliding table, a lifting seat fixed on the vertical sliding table, a horizontal rotating device installed on the lifting seat, a pitching frame installed on the horizontal enlarging device, a pitching device installed on the pitching frame, a rotating frame installed on the pitching device, a rotating device installed on the rotating frame, and a simulation cabin installed on the rotating device; and the control system is respectively connected with the simulation cabin, the transverse moving device, the vertical moving device, the horizontal rotating device, the pitching device and the rotating device and is used for carrying out flight simulation control. The device realizes the simulation of multiple actions through lifting, left-right moving, pitching rotating and left-right rotating, can realize overload simulation, effectively improves the training effect, and has simpler structure and control.
Description
Technical Field
The invention relates to a driving simulation device, in particular to a flight simulation training device.
Background
The cultivation cost of pilots is huge, so the cultivation cost is reduced, usually, a flight simulator is adopted for training, the existing flight simulator mostly adopts a six-degree-of-freedom parallel device for flight simulation, the device is expensive in manufacturing cost and complex in control, overload simulation does not exist, and a continuous load flight simulator cannot provide a flight simulation project of the six-degree-of-freedom parallel device.
Disclosure of Invention
In order to solve the problems, the invention provides a flight simulation training device which is low in cost, simple to control, used for simulating actions such as overturning, pitching, rolling, sharp turning and the like and can realize overload simulation, and the specific technical scheme is as follows:
a flight simulation training device comprising: the portal frame is fixed on the ground; the transverse moving device is fixed on the portal frame; the vertical moving device is fixed on a transverse sliding table of the transverse moving device; the lifting seat is fixed on a vertical sliding table of the vertical moving device; the horizontal rotating device is arranged on the lifting seat; the pitching frame is fixed on the horizontal rotating device; the pitching device is fixed on the pitching frame; a rotating frame mounted on the pitching apparatus; a rotating device mounted on the rotating frame; a simulated cockpit mounted on the rotating device; and the control system is respectively connected with the simulation cabin, the transverse moving device, the vertical moving device, the horizontal rotating device, the pitching device and the rotating device and is used for carrying out flight simulation control.
Further, the lateral moving device includes: the transverse linear guide rails are fixed on the portal frame and are arranged in parallel; the transverse sliding block is slidably mounted on the transverse linear guide rail, and the transverse sliding table is mounted on the transverse sliding block; the transverse screw rod is rotatably arranged on the portal frame; the transverse nut is mounted on the transverse screw rod and connected with the transverse sliding table; and the transverse motor is fixed on the portal frame and is connected with the transverse screw rod.
Further, the vertical moving device includes: the vertical upright posts are symmetrically fixed at two ends of the transverse sliding table; the vertical linear guide rails are fixed on the vertical upright posts and are arranged in parallel; the vertical sliding block is slidably mounted on the vertical linear guide rail, and the vertical sliding table is fixed on the vertical sliding block; the vertical screw rod is rotatably arranged on the vertical upright post; the vertical nut is mounted on the vertical screw rod and connected with the vertical sliding table; and the vertical motor is installed on the vertical upright post and is connected with the vertical screw rod.
Further, the horizontal rotation device includes: the horizontal slewing bearing is fixed on the lifting seat, and the pitching frame is fixed on the horizontal slewing bearing; a horizontal gear engaged with the external teeth of the horizontal slewing bearing; and the rotary motor is connected with the horizontal gear.
Further, the pitching apparatus includes: the pitching speed reducer is fixed on the pitching frame, and an output shaft of the pitching speed reducer is connected with the simulation cabin; and the pitching motor is fixed on the pitching frame and is connected with the pitching speed reducer.
Further, the rotating device includes: a rotary slew bearing mounted on the rotary frame, the simulated cockpit being mounted on the rotary slew bearing; a rotary gear engaged with the external teeth of the rotary slew bearing; and the rotating motor is fixed on the rotating frame and is connected with the rotating gear.
Further, the simulated cockpit comprises: the device comprises an instrument module, a control module, a display module, a sound module, a communication module and a seat.
Further, the control system includes: the upper computer is provided with a flight simulation system; and the CAN bus is respectively connected with the upper computer, the instrument module, the control module, the display module, the communication module and the sound module.
Compared with the prior art, the invention has the following beneficial effects:
the flight simulation training device provided by the invention realizes simulation of various actions through lifting, left-right moving, pitching rotating and left-right rotating, can realize overload simulation, effectively improves training effect, and is simpler in structure and control.
Drawings
FIG. 1 is a schematic structural view of a flight simulation training apparatus;
fig. 2 is a block diagram showing the structure of the flight simulation training apparatus.
Detailed Description
The invention will now be further described with reference to the accompanying drawings.
As shown in fig. 1 and 2, a flight simulation training device includes: the portal frame 1, the portal frame 1 is fixed on the ground; the transverse moving device 2 is fixed on the portal frame 1; the vertical moving device 3 is fixed on the transverse sliding table 21 of the transverse moving device 2; the lifting seat 32 is fixed on the vertical sliding table 31 of the vertical moving device 3; the horizontal rotating device 4, the horizontal rotating device 4 is installed on the lifting seat 32; the pitching frame 51, the pitching frame 51 is fixed on the horizontal rotating device 4; the pitching device 5 is fixed on the pitching frame 51; a rotating frame 61, the rotating frame 61 being mounted on the pitching device 5; a rotating device installed on the rotating frame 61; the simulation cabin 7, the simulation cabin 7 is installed on the rotating device; and the control system is respectively connected with the simulation cabin, the transverse moving device 2, the vertical moving device 3, the horizontal rotating device 4, the pitching device 5 and the rotating device and is used for carrying out flight simulation control.
The lateral movement device 2 includes: the transverse linear guide rails are fixed on the portal frame 1 and are arranged in parallel; the transverse sliding block is arranged on the transverse linear guide rail in a sliding manner, and the transverse sliding table 21 is arranged on the transverse sliding block; the transverse screw rod is arranged on the portal frame 1 through a bearing seat; the transverse nut is arranged on the transverse screw rod and is connected with the transverse sliding table 21; and the transverse motor is fixed on the portal frame 1 and is connected with the transverse screw rod.
The vertical moving device 3 includes: the vertical upright posts are symmetrically fixed at two ends of the transverse sliding table 21; the vertical linear guide rails are fixed on the vertical upright posts and are arranged in parallel; the vertical sliding block is slidably mounted on the vertical linear guide rail, and the vertical sliding table 31 is fixed on the vertical sliding block; the vertical screw rod is arranged on the vertical upright post through a bearing seat; the vertical nut is arranged on the vertical screw rod and is connected with the vertical sliding table 31; and the vertical motor is arranged on the vertical upright post and is connected with the vertical screw rod.
The horizontal turning device 4 includes: the horizontal slewing bearing 41, the horizontal slewing bearing 41 is fixed on the lifting seat 32, the pitching frame 51 is fixed on the horizontal slewing bearing 41; a horizontal gear 44, the horizontal gear 44 meshing with the external teeth of the horizontal slewing bearing 41; and a rotary motor 43, wherein the rotary motor 43 is connected with the horizontal gear 44 and fixed on the lifting seat 32.
The pitching device 5 includes: the pitching speed reducer is fixed on the pitching frame 51, and the output shaft of the pitching speed reducer is connected with the simulation cabin 7; and the pitching motor is fixed on the pitching frame 51 and is connected with the pitching speed reducer.
The pitching frame 51 is a U-shaped frame.
The rotating device includes: a rotary slewing bearing 62, wherein the rotary slewing bearing 62 is arranged on the rotary frame 61, and the simulation cabin 7 is arranged on the rotary slewing bearing 62; a rotary gear 63, the rotary gear 63 meshing with the external teeth of the rotary slew bearing 62; and a rotating motor fixed to the rotating frame 61 and connected to the rotating gear 63.
The simulated cockpit 7 comprises: the device comprises an instrument module, a control module, a display module, a sound module, a communication module and a seat.
Instruments such as a horizon sensor, a magnetic compass, a sideslip sensor and the like are mainly used for indicating flight attitude and heading information of an airplane, and most of the instruments comprise a gyroscope, so that the instruments belong to gyroscope instruments. Because the gyroscope has the axis-fixing property, the attitude angle of the airplane can be conveniently measured, and therefore the horizon sensor is mainly manufactured by utilizing the axis-fixing property of the gyroscope. The design and manufacture of the sideslip instrument mainly depend on the precession principle. The core component of the horizon sensor is a gyroscope inside the horizon sensor, and the horizon sensor is modified by a torquer and a pendulum component in the horizon sensor and is used for measuring the indicators of the pitch attitude angle and the roll angle of an object attached to the gyroscope. The course gyro, the horizon sensor and the sideslip sensor jointly form an attitude indicating system of the airplane. The simulator does not move in the air, the actual gyroscope cannot play the due role, a horizon finder movement mathematical model can be designed by referring to an inertia benchmark program and a gyroscope principle, flight parameters are input into the model as input quantities, attitude and heading parameters including the position, the angle and the like of an aircraft can be calculated, and the attitude and heading instruments are driven by the parameters. The current yaw angle of the aircraft can be obtained by resolving according to a kinetic equation of the aircraft, the current yaw angle is corrected according to longitude and latitude coordinates and altitude information to obtain the true course of the aircraft, the true course which is just obtained is corrected according to magnetic differences of different regions to obtain a magnetic yaw angle, and the magnetic yaw angle is output to a corresponding course instrument.
The control system includes: the upper computer is provided with a flight simulation system; and the CAN bus is respectively connected with the upper computer, the instrument module, the control module, the display module, the communication module and the sound module.
The instrument module is completely the same as a real airplane and provides various flight state information for pilots.
The display module is used for generating various external scenes in the operation process of the airplane and providing real visual perception.
The sound module is used for simulating the sound inside and outside the cabin of real flight and providing vivid sound effect.
The manipulation module is used for providing real manipulation force feeling.
The flight simulation system is the brain of the flight simulation training device, and realizes the resolving of flight actions and the control of each module.
The simulated cockpit 7 carries various simulation devices, the same size as the real cockpit.
The lateral movement means 2, the vertical movement means 3, the horizontal turning means 4, the pitching means 5 and the rotating means are able to simulate the feel of movement of yaw, pitch, roll, lateral, longitudinal and heave during movement of the aircraft, as well as to simulate overload.
The transverse moving device 2 and the vertical moving device 3 are both provided with position control switches for controlling the maximum moving position.
The transverse screw rod is arranged along an X axis, and the vertical screw rod is arranged along a Z axis. The lead screw can adopt a lead screw with a large lead, and all motors adopt servo motors.
The core components of the flight simulation training device comprise a multi-axis motion controller besides a computer for calculating and analyzing real-time data and a flight simulation system. The multi-axis motion controller is used for receiving each driving signal sent by the computer in real time, inputting the driving signal into each servo driver and receiving the feedback of the encoder in the servo motor.
The flight simulation training device has the advantages of high response speed, compact structure, large starting torque, small inertia, high control precision and sensitivity, simple maintenance and simpler control.
During flight simulation, overload simulation can be realized through the transverse screw rod and the vertical screw rod, the screw rod is stable and reliable in transmission, and the linear speed is high; during flight action simulation, the horizontal rotating device 4 rotates around a Z axis, the pitching device 5 rotates around an X axis, and the rotating device rotates around a Y axis; and further, the simulation of the flight action and the overload simulation are realized while the flight action is simulated.
The transverse screw rod is long, and is mainly used for realizing long-time overload simulation. The transverse screw rod can realize overload simulation by reciprocating the transverse sliding table 21. For safety reasons the vertical screw is short, the overload simulation time provided is very short.
The operating system performs transverse movement, vertical movement and rotation around X, Y and a Z axis according to the control of a pilot, and controls the five servo motors to realize the simulation of action and overload, so that the action simulation and the overload simulation are more real, and the problems that an existing continuous load flight simulator in a centrifugal mode can generate an interference angle which is not matched with a simulated airplane in the overload simulation process, the angular motion sensed by the vestibular function of the pilot is not matched with the angular motion sensed by vision due to the existence of the interference angle, the pilot is dizzy, the input control and output feedback of the pilot are not consistent with the simulated airplane and the like are solved.
The pilot controls the control module in the simulation cockpit 7, the control module sends signals to a flight simulation system installed on an upper computer through a CAN bus, the flight simulation system obtains flight state information and control instructions of a flight simulation training device after resolving, the control instructions are transmitted to a transverse motor, a vertical motor, a rotary motor 43, a pitching motor and a rotary motor through the CAN bus, the flight simulation training device generates corresponding movement, the flight state is sent to an instrument module, a display module and a sound module through the CAN bus, and the pilot is provided with real overload, movement, vision and auditory feelings. The angular motion information sensed by the trainee of the flight simulation training device is matched with the angular motion information sensed by the pilot flying the airplane, so that the problem of mismatching between the angular motion sensing and the visual sensing of the trainee of the continuous load flight simulator is effectively solved, and the fidelity of the flight simulation training device is improved.
The flight simulation training device realizes flight simulation in a centralized control mode.
The flight simulation training device can perform a simulation test of large pitching motion. Large pitch movements are mainly related to changes in pitch angle, and roll and yaw angles remain unchanged during the movement. The flight simulation training device keeps a flat flying state at an initial position, then gradually increases the pitch angle, decreases the pitch angle after reaching a certain angle, and finally recovers to the flat flying state.
The flight action of the fighter has strong maneuverability and agility, which is reflected in the wide range change and the rapid conversion of the flight attitude, and the complexity and the intensity of the modern air combat are reflected. The most notable of these flying maneuvers are maneuvered by cobras first created by the well-known pilot, poga and jeff.
The cobra maneuver is an over-stall flying maneuver, and in the flying process, a pilot quickly pulls a control lever backwards to enable the nose of the airplane to face upwards to 110-120 degrees, at the moment, the airplane is in a flat flying state with the tail at the front and the nose at the back, and then pushes the control lever forwards to press the nose, so that the airplane is restored to the original horizontal state. During the cobra maneuver, the entering speed of the airplane is about 425km/h, the airplane decelerates at a speed exceeding 110km/h until the speed is reduced to 148km/h, the airplane is overloaded by 3.5g to 4g in the whole process, and the flying height of the airplane is almost unchanged.
Cobra maneuvers are not only an elegant flight maneuver, but also an effective tactical approach to attack and defense. For example, in air combat using omnidirectional missiles, the enemy plane can be attacked in a wider range by using the missed maneuver, so that more missiles launching opportunities are provided for pilots; when the airplane is subjected to pursuit of an enemy airplane, the motor-driven rapid deceleration of the cobra can be utilized, so that the enemy airplane rushes to the front of the airplane, and a favorable attack position is created for the airplane. Of course, the implementation of such a large pitch delinquent maneuver is not only related to the tactical performance of the fighter, but is also indistinguishable from the pilot's driving technique. Because the traditional flight simulator only has a rotating angle range of plus or minus 35 degrees, the flight action with large pitching can not be finished, and the flight simulation training device provided by the invention can simulate the cobra maneuver through the transverse moving device 2, the vertical moving device 3 and the pitching device 5. The lateral movement means 2 provide a forward deceleration movement and overload, the vertical means provide an upward climb and overload, and the pitch means 5 provide an upward tip of the head.
The technical principle of the present invention is described above in connection with specific embodiments. The description is made for the purpose of illustrating the principles of the invention and should not be construed in any way as limiting the scope of the invention. Based on the explanations herein, those skilled in the art will be able to conceive of other embodiments of the present invention without inventive step, which shall fall within the scope of the appended claims.
Claims (8)
1. A flight simulation training device, comprising:
the portal frame is fixed on the ground;
the transverse moving device is fixed on the portal frame;
the vertical moving device is fixed on a transverse sliding table of the transverse moving device;
the lifting seat is fixed on a vertical sliding table of the vertical moving device;
the horizontal rotating device is arranged on the lifting seat;
the pitching frame is fixed on the horizontal rotating device;
the pitching device is fixed on the pitching frame;
a rotating frame mounted on the pitching apparatus;
a rotating device mounted on the rotating frame;
a simulated cockpit mounted on the rotating device; and
and the control system is respectively connected with the simulation cabin, the transverse moving device, the vertical moving device, the horizontal rotating device, the pitching device and the rotating device and is used for carrying out flight simulation control.
2. A flight simulation training device according to claim 1,
the lateral movement device includes:
the transverse linear guide rails are fixed on the portal frame and are arranged in parallel;
the transverse sliding block is slidably mounted on the transverse linear guide rail, and the transverse sliding table is mounted on the transverse sliding block;
the transverse screw rod is rotatably arranged on the portal frame;
the transverse nut is mounted on the transverse screw rod and connected with the transverse sliding table; and
and the transverse motor is fixed on the portal frame and is connected with the transverse screw rod.
3. A flight simulation training device according to claim 1,
the vertical moving device includes:
the vertical upright posts are symmetrically fixed at two ends of the transverse sliding table;
the vertical linear guide rails are fixed on the vertical upright posts and are arranged in parallel;
the vertical sliding block is slidably mounted on the vertical linear guide rail, and the vertical sliding table is fixed on the vertical sliding block;
the vertical screw rod is rotatably arranged on the vertical upright post;
the vertical nut is mounted on the vertical screw rod and connected with the vertical sliding table; and
the vertical motor is installed on the vertical upright post and is connected with the vertical screw rod.
4. A flight simulation training device according to claim 1,
the horizontal rotation device includes:
the horizontal slewing bearing is fixed on the lifting seat, and the pitching frame is fixed on the horizontal slewing bearing;
a horizontal gear engaged with the external teeth of the horizontal slewing bearing; and
and the rotary motor is connected with the horizontal gear and is fixed on the lifting seat.
5. A flight simulation training device according to claim 1,
the pitching apparatus includes:
the pitching speed reducer is fixed on the pitching frame, and an output shaft of the pitching speed reducer is connected with the simulation cabin; and
the pitching motor is fixed on the pitching frame and connected with the pitching speed reducer.
6. A flight simulation training device according to claim 1,
the rotating device includes:
a rotary slew bearing mounted on the rotary frame, the simulated cockpit being mounted on the rotary slew bearing;
a rotary gear engaged with the external teeth of the rotary slew bearing; and
the rotating motor is fixed on the rotating frame and connected with the rotating gear.
7. A flight simulation training device according to claim 1,
the simulated cockpit comprises: the device comprises an instrument module, a control module, a display module, a sound module, a communication module and a seat.
8. A flight simulation training device according to claim 7,
the control system includes:
the upper computer is provided with a flight simulation system; and
the CAN bus is respectively connected with the upper computer, the instrument module, the control module, the display module, the communication module and the sound module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011528792.1A CN112735223A (en) | 2020-12-22 | 2020-12-22 | Flight simulation training device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011528792.1A CN112735223A (en) | 2020-12-22 | 2020-12-22 | Flight simulation training device |
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| Publication Number | Publication Date |
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| CN112735223A true CN112735223A (en) | 2021-04-30 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202011528792.1A Pending CN112735223A (en) | 2020-12-22 | 2020-12-22 | Flight simulation training device |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115830946A (en) * | 2022-10-28 | 2023-03-21 | 中国航天员科研训练中心 | Multifunctional composite aerospace overload simulation system |
| CN117437828A (en) * | 2023-12-20 | 2024-01-23 | 苏州海易泰克机电设备有限公司 | Rotary cabin, training system and training method thereof |
-
2020
- 2020-12-22 CN CN202011528792.1A patent/CN112735223A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115830946A (en) * | 2022-10-28 | 2023-03-21 | 中国航天员科研训练中心 | Multifunctional composite aerospace overload simulation system |
| CN117437828A (en) * | 2023-12-20 | 2024-01-23 | 苏州海易泰克机电设备有限公司 | Rotary cabin, training system and training method thereof |
| CN117437828B (en) * | 2023-12-20 | 2024-03-29 | 苏州海易泰克机电设备有限公司 | Rotary cabin, training system and training method thereof |
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