CN204087553U - A kind of 360 degree of omnidirectional's overload flight emulation simulators - Google Patents
A kind of 360 degree of omnidirectional's overload flight emulation simulators Download PDFInfo
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Abstract
The utility model discloses a kind of 360 degree of omnidirectional's overload flight emulation simulators, the center of gravity of trainee is the same with real flight course, in the front portion of the center of gravity of airplane.This type of flight simulator comprises oscilaltion system, the first kinematic system, secondary motion requirement, cockpit system four part.Control pitch motor and left rotation and right rotation motor respectively by intelligent control system, the center of gravity front portion in the center of gravity of airplane the same as real flight course of trainee, pilot can experience translation and rotation simultaneously.What comes into a driver's various are rotated through that carrying is dynamic is converted into electric signal, control step motor being synchronized with the movement in X, Y, Z axis by intelligent control system.Implement the utility model and both can reduce training cost, ensure training effect, can flying the training time of the trainees such as flying cadet be reduced again.
Description
Technical field
The utility model relates to fly simulation training facility technology field, is specifically related to a kind of 360 degree of omnidirectional's overload flight emulation simulators.
Background technology
Fly simulation training is exactly will build virtual " truly " flight environment of vehicle to pilot.Here environment mainly refers to two parts: be machine environment on the one hand, i.e. aircraft cockpit, equipment etc.; Be external environment condition on the other hand, mainly refer to natural conditions, geographical conditions etc.In machine environment, be more crucial technology to the simulation of airplane motion, innervation (as acceleration, seat buffeting etc.); Also important to the simulation of the instrument in aircraft cockpit, operating equipment and integrated display system, concerning pilot, passenger cabin must have the sense of reality and presence.In China, people are improving constantly the understanding of flight simulator in the vital role of aviation field, science and technology of aviation and aircraft industry obtain fast development, since " 12 ", along with the quickening of country's open field, low latitude paces, what country helped aircraft industry puts more effort, and domestic flight emulation simulator also gets more and more.Type of flight simulator contributes to the security improving training, contributes to the cost expenses reducing flight training, and contributing to the flight training time, the lifting flight skill that shorten trainee, is the necessary technology means of training aircrew both at home and abroad.
In existing flight simulator, the center of gravity of trainee is arranged on the intersection point of simulator pitching, roll, yawed flight attitude axis, and when this and aircraft flight, the actual conditions of pilot's centre of gravity place are inconsistent.Actual conditions are when aircraft flight, pilot's center of gravity usually in the front end of aircraft, therefore when aircraft carry out rolling, roll, swing time, pilot can experience translation and rotation simultaneously.Simultaneously, existing flight simulator cockpit can only simulate the simulated actions such as inclination, by a small margin swing by a small margin in a plane, such as existing six degree of freedom flight simulator cockpit generally adopts Stewart platform structure, Stewart platform structure can only simulate the simulated actions such as rolling, roll, significantly swing in a plane, the compound actions such as 360 degree of omnidirectional's overloads and special type danger cannot be realized, be difficult to ensure training effect.Existing flight simulator systems what comes into a driver's produces mainly through projection pattern, projector is by air objective, in flight course pilot look out of my cabin actual scenery live fluoroscopic on the ball curtain of flight simulator, the rolling of existing simulator, roll, the motion such as swing is in a plane, range of movement is little, simulate rolling and significantly swing time, screen can rotate together along with cockpit, although meet the needs of visual exercise effect, but lack Live Flying to experience, the what comes into a driver's picture emulation property immersed is not high, fidelity is bad, simulated training and practical flight disconnect.
Utility model content
In order to the defect that centre of gravity place actual conditions when solving Stewart platform structure flight simulator trainee's center of gravity and aircraft flight in prior art are not inconsistent, the utility model provides a kind of 360 degree of omnidirectional's overload flight emulation simulators, trainee's center of gravity is the same with real flight course, in the front portion of the center of gravity of airplane.This type of flight simulator mainly comprises oscilaltion system, the first kinematic system, secondary motion requirement, cockpit system four part.
The technical scheme that the utility model adopts:
A kind of 360 degree of omnidirectional's overload flight emulation simulators, is characterized in that: comprise
Oscilaltion system, for the oscilaltion campaign of simulated aircraft;
First kinematic system, for 360 degree, the front and back luffing of simulated aircraft; Described oscilaltion system is connected with the first kinematic system by pitch bearing; Described first kinematic system drives described emulation simulator to complete the luffing of 360 degree, front and back under the driving of pitching drive motor;
Secondary motion requirement, for the rotary motion within the scope of 360 degree to the left or to the right of simulated aircraft; Described first kinematic system is connected with described secondary motion requirement by roll bearing;
Cockpit system, the head cockpit of described cockpit system is fixed on the front end of the roll support bar in described secondary motion requirement, and described cockpit internal system is integrated with automatic counter-balanced system and built-in visual system.
Described oscilaltion system comprises support platform, lifting electric support bar, bearing diagonal electric rod, bearing diagonal electric rod linked set and lifting electric support bar linked set; Described support platform is as the base of whole type of flight simulator, the bottom of described lifting electric support bar is connected to described lifting electric support bar linked set, described lifting electric support bar linked set is fixed in described support platform, described bearing diagonal electric rod one end is connected to described lifting electric support bar, the other end is connected to bearing diagonal electric rod linked set, and described bearing diagonal electric rod linked set is fixed in described support platform.
Described oscilaltion system also comprises gag lever post, and described gag lever post is fixed in described support platform, and described gag lever post and described bearing diagonal electric rod separate from described lifting electric support bar both sides.
Described first kinematic system comprises pitching drive motor, pitch bearing and pitching support bar; Described pitching support bar is connected with lifting electric support bar by pitch bearing; Described pitching drive motor is fixed on the two ends of described pitching support bar by the axle sleeve of self.
Described secondary motion requirement comprises pitching support bar linked set, tail counterweight cabin, roll drive motor and roll support bar; Described roll support bar is assemblied on pitching support bar by pitching support bar linked set, described roll support bar and the cross-shaped state of described pitching support bar; Described tail counterweight cabin is connected with described roll support bar; Described tail counterweight cabin is built-in with deck store automatic counter-balanced system.
Described deck store automatic counter-balanced system is by sensor senses pilot or trainee's body weight information, the position of tail counterweight cabin on roll support bar is regulated according to pilot's body weight information self-adapting, after adjustment, roll support bar enters immediately from locking state, location passenger cabin, avoids passenger cabin to tilt to fall.
Described cockpit internal system is also provided with attitude operating rod and QUADRANT, and described attitude operating rod control imitation simulator does luffing and/or roll motion.
Described built-in visual system receives relevant cabin body attitude information, and chain of command keeps forward vertical with ground to the screen-picture of pilot all the time.
The utility model technique effect:
The utility model proposes a kind of 360 degree of omnidirectional's overload flight emulation simulators, this type of flight simulator controls pitch motor and left rotation and right rotation motor respectively by the intelligent control system (also can be parametric controller server) being positioned at cabin, achieve true aircraft is rolled in flight course, roll, the action such as swing analogue simulation, i.e. 360 degree of omnidirectional's overload flight analogue simulations.Use type of flight simulator described in the utility model, the center of gravity of trainee is the same with real flight course, and in the front portion of the center of gravity of airplane, therefore trainee can experience translation and rotation simultaneously.Meanwhile, what comes into a driver's various are rotated through that carrying is dynamic is converted into electric signal, control step motor being synchronized with the movement in X, Y, Z axis by intelligent control system, realize the synchronous of the high property immersed what comes into a driver's picture and 360 degree of any compound motions of omnidirectional.360 degree of omnidirectional movings comprise X, Y, Z three-axis moving, along X, Y, Z tri-axle rotary motion and compound motion arbitrarily, and 360 rotary motion and overload and extraordinary dangerous sports, can for participant multiple flying condition is provided under flying-vision comparatively true to nature and sensation when participating in the cintest, both training cost can be reduced, ensure training effect, and can flying the training time of the trainees such as flying cadet be reduced.
Accompanying drawing explanation
Fig. 1 is the utility model 360 degree of omnidirectional's overload flight emulation simulator structural representations.
Fig. 2 is visual system schematic diagram in the utility model 360 degree of omnidirectional's overload flight emulation simulator driving cabins and passenger cabin.
Fig. 3 is the built-in visual system schematic diagram of the helmet, and being that both can be used alone also can be supporting with visual system in passenger cabin, is the upgrade version of visual system in passenger cabin.
Reference numeral is as follows: 1-support platform, 2-lifting electric support bar, 3-bearing diagonal electric rod, 4-bearing diagonal electric rod linked set, 5-gag lever post, 6-lifting electric support bar linked set, 7-pitching drive motor, 8-pitch bearing, 9-pitching support bar, 10-pitching support bar linked set, 11-tail counterweight cabin, 12-roll drive motor, 13-roll support bar, 14-head cockpit.
Embodiment
The center of gravity of existing flight simulator trainee is on the intersection point of simulator pitching, roll, yawed flight attitude axis, and pilot (i.e. trainee) is difficult to when simulation is undergone training experience translation and rotation simultaneously.And actual conditions are when aircraft flight, pilot's center of gravity usually in the front end of aircraft, therefore when aircraft carry out rolling, roll, swing time, pilot (or trainee) can experience translation and rotation simultaneously.The technical matters that the utility model solves is, by providing a kind of 360 degree of omnidirectional's overload flight emulation simulators, the analogue simulation of the actions such as realization is rolled in flight course to true aircraft, roll, swing, i.e. 360 degree of omnidirectional's overload flight analogue simulations.For trainee provides the flight experience experiencing translation and rotation simultaneously; Meanwhile, the synchronous of the high property immersed what comes into a driver's picture and 360 degree of any compound motions of omnidirectional is realized.
Below in conjunction with accompanying drawing, embodiment of the present utility model is described further.
Main flow flight simulator common at present has Stewart platform structure.Although Stewart platform structure has symmetrical structure, have six-freedom degree, structure is simple, is applicable to modularized production.But the center of gravity of trainee overlaps with the center of gravity of Stewart flight simulator, be not inconsistent with the actual conditions of pilot's center of gravity before the center of gravity of airplane in practical flight process, and Stewart platform structure flight simulator can only simulate the simulated actions such as rolling, roll, significantly swing in a plane, the analogue simulation of 360 degree of omnidirectional's overloads and the dangerous compound action of special type and extraordinary dangerous situation more cannot be realized.Therefore, when simulated aircraft carry out rolling, roll, swing time, trainee's impression is tested less than practical flight healths such as the translation in Live Flying process and rotations.
Fig. 1 is the utility model 360 degree of omnidirectional's overload flight emulation simulator structural representations.Fig. 2 is visual system schematic diagram in the utility model 360 degree of omnidirectional's overload flight emulation simulator driving cabins and passenger cabin.
The utility model discloses a kind of type of flight simulator with 360 degree of omnidirectional's overload analog capabilities, this type of flight simulator mainly comprises oscilaltion system, the first kinematic system, secondary motion requirement and cockpit system four part.Oscilaltion system is connected with the first kinematic system by pitch bearing, first kinematic system is connected with secondary motion requirement by roll bearing, the cockpit system integration automatic counter-balanced system and built-in visual system, automatic counter-balanced system is according to the position of pilot (i.e. trainee) body weight Automatic adjusument counterweight tail counterweight cabin (can be a balancing weight), built-in visual system is by the underriding of cabin controlling system by built-in visual system flying scene, spiral, climb, the overloads such as roll or non-overloaded flight are converted into control electric signal, control electric signal and accurately control pitch motor, left rotation and right rotation motor, a year flight training is spent by the omnidirectional 360 realizing flight simulator.360 degree of omnidirectional movings described in the utility model comprise X, Y, Z three-axis moving, along X, Y, Z tri-axle rotary motion and any compound motion, and 360 degree rotary motions and transshipping and extraordinary dangerous sports.Overload described in the utility model refers to the ratio of the acceleration that the power except gravity on aircraft or pilot's health of acting on produces and gravity acceleration constant.
As shown in Figure 1, oscilaltion system comprises support platform 1, lifting electric support bar 2, bearing diagonal electric rod 3, bearing diagonal electric rod linked set 4, gag lever post 5 and lifting electric support bar linked set 6.Support platform 1 is the base of whole type of flight simulator, the lifting electric support bar linked set 6 of lifting electric support bar 2 by being positioned at bottom lifting electric support bar 2, on support platform 1 table top is connected with support platform 1, support platform 1 being fixed with oscilaltion drive motor, being arranged on oscilaltion drive motor in support platform 1 for driving lifting electric support bar 2, bearing diagonal electric rod 3 associated movement.Bearing diagonal electric rod 3 is connected with support platform 1 by bearing diagonal electric rod linked set 4; Gag lever post 5 is fixed in described support platform 1, separates from described lifting electric support bar both sides with described bearing diagonal electric rod 3.Gag lever post 5 is fixed in support platform 1 by nut, plays restriction lifting electric support bar 2 and crosses the effect of facing upward.Oscilaltion drive motor and lifting electric support bar 2 are one, and be positioned at the lower end of lifting electric support bar 2, whole lifting electric support bar 2 is from locked system when not moving, and enters from locking state, prevents driving stem landing, causes passenger cabin to fall.Visible, the oscilaltion system of the utility model 360 degree of omnidirectional's overload flight emulation simulators achieves the oscilaltion campaign of type of flight simulator.
First kinematic system comprises pitching drive motor 7, pitch bearing 8 and pitching support bar 9.Pitching support bar 9 is connected with lifting electric support bar 2 by pitch bearing 8, and that is, the first kinematic system is connected with the first kinematic system by pitch bearing 8; Pitching drive motor 7 is fixed on the two ends of pitching support bar 9 by the axle sleeve of self; Pitching drive motor 7 can realize 360 degree of rotary motions around pitching support bar 9.First kinematic system, under the driving of pitching drive motor 7, drives type of flight simulator described in the utility model to complete the luffing of 360 degree, front and back.
Secondary motion requirement comprises pitching support bar linked set 10, tail counterweight cabin 11, roll drive motor 12 and roll support bar 13.Roll support bar 13 is assemblied on pitching support bar 9 by pitching support bar linked set 10, achieves the interconnected of secondary motion requirement and the first kinematic system with this.Tail counterweight cabin 11 is connected with roll support bar 13, tail counterweight cabin 11 is built-in with deck store automatic counter-balanced system, this deck store automatic counter-balanced system is by sensor senses occupant (i.e. trainee) weight, then can, according to the position of occupant (i.e. trainee) body weight automatic regulating machine tail counterweight cabin 11 on roll support bar 13, be the balance device of the utility model 360 degree of omnidirectional's overload flight emulation simulators.
Cockpit system comprises head cockpit 14 and built-in visual system.Head cockpit 14 is fixed on the front end of roll support bar 13, built-in visual system by the cabin controlling system of head cockpit 14 by the underriding of built-in visual system flying scene, spiral, climb, the overload such as roll or non-overloaded flight is converted into control electric signal, control signal accurately controls pitch motor, left rotation and right rotation motor, makes it to drive flight simulator described in the utility model to complete the action such as pitch, left rotation and right rotation.Described secondary motion requirement and the acting in conjunction of described cockpit system, a year flight training is spent by the omnidirectional 360 realizing flight simulator.
Fig. 3 is the built-in visual system schematic diagram of the helmet, and being that namely can be used alone also can be supporting with visual system in passenger cabin, is the upgrade version of visual system in passenger cabin.The built-in visual system of the helmet also claims built-in visual system.But that according to real experiences tries on, its resolution cannot meet request for utilization, and reason is exactly easily cause trainee dizzy.Usually, trainee needs to wear the helmet similar to Figure 3 when receiving fly simulation training, and the inside is provided with the built-in visual system of the helmet.
The built-in visual system that the utility model adopts can reproduce physiographic relief landforms (mountains and rivers, river, forest, ocean, sky etc.) in true environment and the places of cultural interest (town buildings, bridge, highway, railway, airport etc.), scene round the clock under the multiple meteorological condition such as rain, snow is provided simultaneously, creation one is very dangerous, no matter how passenger cabin overturns, picture keeps forward plumbness with ground all the time, is close to real three-dimensional flight environment of vehicle.
As shown in Figure 1, show that on the one hand the utility model 360 degree of omnidirectional's overload flight emulation simulators both can oscilaltion campaign, also can do 360 degree of roll motions.The roll support bar 13 of the utility model simulator is assemblied on 9 pitching support bars by 10 pitching support bar linked sets, achieves the interconnected of secondary motion requirement and the first kinematic system, around the cylinder 360 degree rotation at lifting electric support bar 2 place.
Lifting electric support bar 2 controls type of flight simulator and completes oscilaltion campaign, movement velocity and acceleration adjustable, suppose that moving mass quality is m, the accelerometer of requirement is a, then the hydraulic pressure that the lifting electric support bar 2 required produces/electromagnetism lifting force is:
F＝ma
Requirement power is:
That is: the power of requirement is with to realize maximum speed limit relevant.
The utility model 360 degree of omnidirectional's overload flight emulation simulator structural representations also demonstrate the course motion conditions of body, and wherein motor (specifically referring to pitching motor and roll motor) driving power requires also relevant with angular acceleration with body maximum limit fixed angular speed.The cockpit system integration automatic counter-balanced system and built-in visual system, tail counterweight cabin carries out automatic weighing design, automatic counter-balanced system is according to the position in operator's body weight Automatic adjusument counterweight tail counterweight cabin.When the adjustment of configuration is machine on simulator powers up, counterweight cabin Rigen, according to balance sensor, regulates balance position automatically, make to reach static balancing before and after passenger cabin and counterweight cabin, automatic adjustment, the motor rate therefore required is lower, only needs the restriction depending on setup time to determine.From locked system as a kind of safety practice, after automatic counter-balanced system fading margin process, whole driving stem is from locked system when not moving, and prevents driving stem landing, causes passenger cabin to fall.Play Anti-inclining, fall arrest effect.
Fig. 1 also demonstrates the situation of the utility model luffing, and be made up of point bilateral pitch bearing, gear and a pitching drive motor 7 etc. that the pitch bearing 8 being listed in simulator the right and left is formed, pitching drive motor 7 moment has following formula to determine:
2H
θ＝[I]
θω
θ
Wherein [I]
θfor the inertial tensor of luffing,
Meanwhile, the roll drive motor that the roll motion of flight simulator body is linked by roll support bar and body controls, and the moment that motor will provide is:
H
γ＝[I]
γω
γ
Wherein [I]
γfor the inertial tensor of roll motion, the power of motor obviously required is closely related with roll angle speed.
Stewart platform structure also comprises Stewart control system usually; Stewart control system makes trainee be fixed on seat, and seat is fixing, by controlling the motion of operating rod control simulation cabin body; obtain associ-ated motion parameters, result is delivered to projection screen display.The main parameter calculation of system is all calculate at single computer internal simulation, not complicated drive system.
Intelligent control system in the driving cabin of the utility model 360 degree of omnidirectional's overload flight emulation simulators adds the design of the information interaction of people and cabin body on the basis of general gesture stability, passenger cabin visual system does not adopt projection pattern, but the aircraft flight motion directly shown in the omnibearing artificial actual environment of emulated interface, can the motion of adjusting cabin body, make trainee's true feeling be subject to state of flight.
360 degree of omnidirectional's type of flight simulators that the utility model provides, pitch motor and left rotation and right rotation motor is controlled respectively by intelligent control system, the center of gravity front portion in the center of gravity of airplane the same as real flight course of trainee, what comes into a driver's various are rotated through that carrying is dynamic is converted into electric signal, control step motor being synchronized with the movement in X, Y, Z axis by intelligent control system.Because human body rolls up and down, what comes into a driver's device also rolls up and down along with the synchronous left and right of trainer, but the display frame in what comes into a driver's obtains along with control system reverse resolution, makes what comes into a driver's picture keep vertical with ground all the time like this; When really flying with pilot on high in the picture seen be consistent.Implement the utility model and both can reduce training cost, ensure training effect, can flying the training time of the trainees such as flying cadet be reduced again.
It should be pointed out that the above embodiment can make those skilled in the art's comprehend the utility model create, but limit the utility model creation never in any form.Therefore; although this instructions has been described in detail the utility model creation with reference to drawings and Examples; but; those skilled in the art are to be understood that; still can create the utility model and modify or equivalent replacement; in a word, all do not depart from technical scheme and the improvement thereof of the spirit and scope that the utility model is created, and it all should be encompassed in the utility model and create in the middle of the protection domain of patent.
Claims (8)
1. 360 degree of omnidirectional's overload flight emulation simulators, is characterized in that: comprise
Oscilaltion system, for the oscilaltion campaign of simulated aircraft;
First kinematic system, for 360 degree, the front and back luffing of simulated aircraft; Described oscilaltion system is connected with the first kinematic system by pitch bearing; Described first kinematic system drives described emulation simulator to complete the luffing of 360 degree, front and back under the driving of pitching drive motor;
Secondary motion requirement, for the rotary motion within the scope of 360 degree to the left or to the right of simulated aircraft; Described first kinematic system is connected with described secondary motion requirement by roll bearing;
Cockpit system, the head cockpit of described cockpit system is fixed on the front end of the roll support bar in described secondary motion requirement, and described cockpit internal system is integrated with automatic counter-balanced system and built-in visual system.
2. 360 degree of omnidirectional's overload flight emulation simulators according to claim 1, it is characterized in that: described oscilaltion system comprises support platform, lifting electric support bar, bearing diagonal electric rod, bearing diagonal electric rod linked set and lifting electric support bar linked set; Described support platform is as the base of whole type of flight simulator, the bottom of described lifting electric support bar is connected to described lifting electric support bar linked set, described lifting electric support bar linked set is fixed in described support platform, described bearing diagonal electric rod one end is connected to described lifting electric support bar, the other end is connected to bearing diagonal electric rod linked set, and described bearing diagonal electric rod linked set is fixed in described support platform.
3. 360 degree of omnidirectional's overload flight emulation simulators according to claim 2, it is characterized in that: described oscilaltion system also comprises gag lever post, described gag lever post is fixed in described support platform, and described gag lever post and described bearing diagonal electric rod separate from described lifting electric support bar both sides.
4. 360 degree of omnidirectional's overload flight emulation simulators according to claim 1, is characterized in that: described first kinematic system comprises pitching drive motor, pitch bearing and pitching support bar; Described pitching support bar is connected with lifting electric support bar by pitch bearing; Described pitching drive motor is fixed on the two ends of described pitching support bar by the axle sleeve of self.
5. 360 degree of omnidirectional's overload flight emulation simulators according to claim 1, is characterized in that: described secondary motion requirement comprises pitching support bar linked set, tail counterweight cabin, roll drive motor and roll support bar; Described roll support bar is assemblied on pitching support bar by pitching support bar linked set, described roll support bar and the cross-shaped state of described pitching support bar; Described tail counterweight cabin is connected with described roll support bar; Described tail counterweight cabin is built-in with deck store automatic counter-balanced system.
6. 360 degree of omnidirectional's overload flight emulation simulators according to claim 5, it is characterized in that: described deck store automatic counter-balanced system is by sensor senses pilot or trainee's body weight information, the position of tail counterweight cabin on roll support bar is regulated according to pilot's body weight information self-adapting, after adjustment, roll support bar enters immediately from locking state, location passenger cabin, avoids passenger cabin to tilt to fall.
7. 360 degree of omnidirectional's overload flight emulation simulators according to claim 6, it is characterized in that: described cockpit internal system is also provided with attitude operating rod and QUADRANT, described attitude operating rod control imitation simulator does luffing and/or roll motion.
8. 360 degree of omnidirectional's overload flight emulation simulators according to claim 7, is characterized in that: described built-in visual system receives relevant cabin body attitude information, and chain of command keeps forward vertical with ground to the screen-picture of pilot all the time.
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Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN103886782A (en) * | 2014-04-09 | 2014-06-25 | 陈京波 | 360-degree omni-directional overload flight simulator |
| CN104616562A (en) * | 2015-02-16 | 2015-05-13 | 清华大学 | Rail type flight simulator having continuous overload simulation capability |
| CN104880962A (en) * | 2015-05-28 | 2015-09-02 | 清华大学 | Dynamic flight simulator real time motion control method |
| CN105654809A (en) * | 2016-01-10 | 2016-06-08 | 王建雄 | Full-angle aviation simulation equipment |
| CN105791754A (en) * | 2015-05-07 | 2016-07-20 | 寺坂立 | Aircraft remote control system |
| CN106110660A (en) * | 2016-08-15 | 2016-11-16 | 西安翔辉仿真科技有限公司 | Three 360 degree of axles comprehensive high speed sensation simulation emulator |
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| CN110767027A (en) * | 2019-11-11 | 2020-02-07 | 中国人民解放军第四军医大学 | Pilot space situation perception auxiliary training system |
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| CN103886782A (en) * | 2014-04-09 | 2014-06-25 | 陈京波 | 360-degree omni-directional overload flight simulator |
| CN104616562A (en) * | 2015-02-16 | 2015-05-13 | 清华大学 | Rail type flight simulator having continuous overload simulation capability |
| CN105791754A (en) * | 2015-05-07 | 2016-07-20 | 寺坂立 | Aircraft remote control system |
| CN105791754B (en) * | 2015-05-07 | 2018-10-30 | 寺坂立 | The joystick system of aircraft |
| CN104880962B (en) * | 2015-05-28 | 2017-10-03 | 清华大学 | A kind of Dynamic Flight Simulator real time kinematics control method |
| CN104880962A (en) * | 2015-05-28 | 2015-09-02 | 清华大学 | Dynamic flight simulator real time motion control method |
| CN105654809A (en) * | 2016-01-10 | 2016-06-08 | 王建雄 | Full-angle aviation simulation equipment |
| CN106110660B (en) * | 2016-08-15 | 2018-06-26 | 西安翔辉仿真科技有限公司 | Three axis 360 degrees omnidirection high speed sensation simulation emulators |
| CN106110660A (en) * | 2016-08-15 | 2016-11-16 | 西安翔辉仿真科技有限公司 | Three 360 degree of axles comprehensive high speed sensation simulation emulator |
| CN110313763A (en) * | 2019-06-27 | 2019-10-11 | 恒昌工業有限公司 | The model aircraft bracket and model aircraft of multi-angle rotary fight maneuver device |
| CN110313763B (en) * | 2019-06-27 | 2020-11-13 | 恒昌工業有限公司 | Multi-angle rotating's aircraft model support and aircraft model fight exercise device |
| CN110767027A (en) * | 2019-11-11 | 2020-02-07 | 中国人民解放军第四军医大学 | Pilot space situation perception auxiliary training system |
| CN110767027B (en) * | 2019-11-11 | 2021-08-20 | 中国人民解放军第四军医大学 | Pilot space situation perception auxiliary training system |
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