CN102013188A - Centrifugal machine based flight simulation system and method thereof - Google Patents
Centrifugal machine based flight simulation system and method thereof Download PDFInfo
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- CN102013188A CN102013188A CN 201010575227 CN201010575227A CN102013188A CN 102013188 A CN102013188 A CN 102013188A CN 201010575227 CN201010575227 CN 201010575227 CN 201010575227 A CN201010575227 A CN 201010575227A CN 102013188 A CN102013188 A CN 102013188A
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Abstract
The invention relates to a centrifugal machine based flight simulation system and a method thereof. The system comprises a control cabin (2), a data processing system (3) and a multi-dimensional centrifugal machine (1), wherein the control cabin (2) is internally provided with an image display device (5) and a flight control device (5), a pilot outputs a control signal to the data processing system (3) by operating the flight control device (5), and the control signal output terminal of the data processing system (3) drives the control cabin (2) to rotate by controlling rotation of the multi-dimensional centrifugal machine (1). The invention utilizes the multi-dimensional centrifugal machine to increase duration of body feeling gravity acceleration, and rotating speed and steering of two drive motors of the multi-dimensional centrifugal machine are changed, so as to change rotation in horizontal and vertical dimensions, thus the effect closer to the real can be realized compared with the effect of like products.
Description
Technical field
The present invention relates to a kind of flight simulation system, specifically relates to a kind of flight simulation system based on hydro-extractor.
Background technology
Along with development of aviation and aerospace technology, because real flight training has very big danger, in order to make the break-in of flight student pilot's sense of reality aircraft in flight course, overweight or the weightless experience that speed change is brought, people utilize and centrifugally bring lasting overweight impression to the trainer, but hydro-extractor only provides the variation of simple body sense acceleration of gravity.Simultaneously, various flight simulators are arranged also, also have 3D helmet analog vision in conjunction with some 3D simulation softwards, most of simulators are to jolt with the hydraulic stem generation of bottom, come the speed change of simulated flight, but its duration is not enough, can not goes out aloft impression by real simulation.
Summary of the invention
The objective of the invention is at deficiency of the prior art, a kind of flight simulation system based on hydro-extractor is provided, when lasting body sense acceleration of gravity is provided, also visually give real impression.
Technical scheme of the present invention is:
A kind of flight simulation system based on hydro-extractor, it comprises control passenger cabin, data handling system and multidimensional hydro-extractor, be provided with image display and flight control unit in the described control passenger cabin, the control signal output ends of flight control unit links to each other with the signal input end of data handling system, and the control signal output ends of data handling system drives the rotation of control passenger cabin by the rotation of control multidimensional hydro-extractor.
A kind of flight simulation method based on hydro-extractor, it may further comprise the steps: the pilot enters in the control passenger cabin, opens flight control unit, selects corresponding emulation mode, image display display simulation system preview image; The pilot exports control signal to data handling system by the operation flight control unit, and data handling system is handled the back changes the control passenger cabin by the rotation of control multidimensional hydro-extractor running.
Multidimensional hydro-extractor of the present invention comprises vertical drive motor, the horizontal drive motor, vertically rotating shaft, horizontal rotating shaft and rotating base, the vertical drive motor of multidimensional hydro-extractor drives vertical rotating shaft rotation, one end of this vertical rotating shaft is fixed with the control passenger cabin, drive the rotation of control passenger cabin vertical direction, the rotation of horizontal drive driven by motor horizontal rotating shaft, one end of horizontal rotating shaft is connected with the rotation center of rotating base, the rotation of driven rotary base, this rotating base is provided with a gangbar, one end of gangbar links to each other with rotating base, the other end links to each other with vertical rotating shaft, drives the rotation of control passenger cabin horizontal direction by vertical rotating shaft.
Data handling system of the present invention turns in addition by vertical drive motor, the horizontal drive rotating speed of motor that changes the multidimensional hydro-extractor, changes the multidimensional hydro-extractor in level and the vertically rotation of dimension.
Image display of the present invention is the three-dimensional helmet or three dimensional display.
Beneficial effect of the present invention:
The present invention utilizes the multidimensional hydro-extractor that the duration of proper sense acceleration of gravity is increased; The acceleration of simulation is free more controlled on direction, and the rotating speed of two drive motor by changing the multidimensional hydro-extractor turns in addition, comes change level and the vertically rotation of dimension, than like product more near real effect.
Description of drawings
Fig. 1 is a theory diagram of the present invention.
Fig. 2 is a structural representation of the present invention.
Embodiment
The present invention is further illustrated below in conjunction with drawings and Examples.
As shown in Figure 1, a kind of flight simulation system based on hydro-extractor, it comprises control passenger cabin 2, data handling system 3(processor chips model is Intel Core i7 980X Extreme Edition, GPU:NVIDIA GTX580 SLI) and multidimensional hydro-extractor 1, be provided with image display 5 and flight control unit 5 in the described control passenger cabin 2, the control signal output ends of flight control unit 5 links to each other with the signal input end of data handling system 3, and the control signal output ends of data handling system 3 drives 2 rotations of control passenger cabin by the rotation of control multidimensional hydro-extractor 1.
Multidimensional hydro-extractor 1 of the present invention comprises vertical drive motor 6, horizontal drive motor 7, vertically rotating shaft 8, horizontal rotating shaft 9 and rotating base 10, the vertical drive motor 6 of multidimensional hydro-extractor 1 drives vertical rotating shaft 8 rotations, one end of this vertical rotating shaft 8 is fixing with control passenger cabin 2, drive the rotation of control passenger cabin 2 vertical directions, horizontal drive motor 7 drives horizontal rotating shaft 9 rotations, one end of horizontal rotating shaft 9 is connected with the rotation center of rotating base 10,10 rotations of driven rotary base, this rotating base 10 is provided with a gangbar 11, one end of gangbar 11 links to each other with rotating base 10, the other end links to each other with vertical rotating shaft 8, drives the rotation of control passenger cabin 2 horizontal directions by vertical rotating shaft 8.
A kind of flight simulation method of the flight simulation system based on hydro-extractor, it may further comprise the steps: the pilot enters in the control passenger cabin 2, opens flight control unit 5, selects corresponding emulation mode, image display 5 display simulation systems preview image; The pilot exports control signal to data handling system 3 by operation flight control unit 5, and data handling system 3 is handled the back changes control passenger cabin 2 by the rotation of control multidimensional hydro-extractor 1 running.
During concrete enforcement:
Multidimensional hydro-extractor 1 rotation in level and perpendicular by vertical drive motor 6 and horizontal drive motor 7 provides omnibearing acceleration to experience.Data handling system 3 with the current acceleration information of the aircraft that simulates real-time pass to multidimensional hydro-extractor 1.By changing the velocity of rotation of multidimensional hydro-extractor 1 at surface level, provide acceleration on the fore-and-aft direction to the people, by changing the velocity of rotation of multidimensional hydro-extractor 1, provide side direction and acceleration above-below direction to the people at vertical direction.Multidimensional hydro-extractor 1 carries out the computer simulation of flying quality and Flame Image Process by data handling system 3 and to the control of multidimensional hydro-extractor 1, image information is transferred in the three-dimensional helmet 4, flight control unit 5 links to each other with data handling system 3 simultaneously, and the transmission people is to the control signal of the aircraft of simulation.Wherein the rotating speed of two drive motor by changing multidimensional hydro-extractor 1 turns in addition, changes the acceleration of a plurality of dimensions.
The part that the present invention does not relate to prior art that maybe can adopt all same as the prior art is realized.
Claims (7)
1. flight simulation system based on hydro-extractor, it is characterized in that it comprises control passenger cabin (2), data handling system (3) and multidimensional hydro-extractor (1), be provided with image display (5) and flight control unit (5) in the described control passenger cabin (2), the control signal output ends of flight control unit (5) links to each other with the signal input end of data handling system (3), and the control signal output ends of data handling system (3) drives control passenger cabin (2) rotation by the rotation of control multidimensional hydro-extractor (1).
2. according to the described flight simulation system of claim 1 based on hydro-extractor, it is characterized in that described multidimensional hydro-extractor (1) comprises vertical drive motor (6), horizontal drive motor (7), vertically rotating shaft (8), horizontal rotating shaft (9) and rotating base (10), the vertical drive motor (6) of multidimensional hydro-extractor (1) drives vertical rotating shaft (8) rotation, one end of this vertical rotating shaft (8) is fixing with control passenger cabin (2), drive the rotation of control passenger cabin (2) vertical direction, horizontal drive motor (7) drives horizontal rotating shaft (9) rotation, one end of horizontal rotating shaft (9) is connected with the rotation center of rotating base (10), driven rotary base (10) rotation, this rotating base (10) is provided with a gangbar (11), one end of gangbar (11) links to each other with rotating base (10), the other end links to each other with vertical rotating shaft (8), drives the rotation of control passenger cabin (2) horizontal direction by vertical rotating shaft (8).
3. according to the described flight simulation system of claim 1, it is characterized in that described image display (5) is the three-dimensional helmet or three dimensional display based on hydro-extractor.
4. based on the flight simulation method of the described flight simulation system based on hydro-extractor of claim 1, it is characterized in that it may further comprise the steps: the pilot enters in the control passenger cabin (2), open flight control unit (5), select corresponding emulation mode, image display (5) display simulation system preview image; The pilot exports control signal to data handling system (3) by operation flight control unit (5), and data handling system (3) is handled the back changes control passenger cabin (2) by the rotation of control multidimensional hydro-extractor (1) running.
5. the flight simulation method of stating according to claim 4 based on hydro-extractor, it is characterized in that described multidimensional hydro-extractor (1) comprises vertical drive motor (6), horizontal drive motor (7), vertically rotating shaft (8), horizontal rotating shaft (9) and rotating base (10), the vertical drive motor (6) of multidimensional hydro-extractor (1) drives vertical rotating shaft (8) rotation, one end of this vertical rotating shaft (8) is fixing with control passenger cabin (2), drive the rotation of control passenger cabin (2) vertical direction, horizontal drive motor (7) drives horizontal rotating shaft (9) rotation, one end of horizontal rotating shaft (9) is connected with the rotation center of rotating base (10), driven rotary base (10) rotation, this rotating base (10) is provided with a gangbar (11), one end of gangbar (11) links to each other with rotating base (10), the other end links to each other with vertical rotating shaft (8), drives the rotation of control passenger cabin (2) horizontal direction by vertical rotating shaft (8).
6. the flight simulation method based on hydro-extractor according to claim 5, it is characterized in that described data handling system (3) turns in addition by the vertical drive motor (6) that changes multidimensional hydro-extractor (1), the rotating speed of horizontal drive motor (7), change multidimensional hydro-extractor (1) in level and the vertically rotation of dimension.
7. the flight simulation method based on hydro-extractor according to claim 4 is characterized in that described image display (5) is the three-dimensional helmet or three dimensional display.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010105752270A CN102013188B (en) | 2010-12-06 | 2010-12-06 | Centrifugal machine based flight simulation system and method thereof |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010105752270A CN102013188B (en) | 2010-12-06 | 2010-12-06 | Centrifugal machine based flight simulation system and method thereof |
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| Publication Number | Publication Date |
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| CN102013188A true CN102013188A (en) | 2011-04-13 |
| CN102013188B CN102013188B (en) | 2012-07-18 |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104464441A (en) * | 2014-12-24 | 2015-03-25 | 喻明 | Flight simulation training device |
| CN105791754A (en) * | 2015-05-07 | 2016-07-20 | 寺坂立 | Aircraft remote control system |
| CN111785126A (en) * | 2020-07-27 | 2020-10-16 | 中国工程物理研究院总体工程研究所 | Body rotation illusion simulation method integrating visual information and motion perception |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101339701A (en) * | 2008-08-18 | 2009-01-07 | 吉林大学 | Three freedom degree movement simulation platform |
| CN201540661U (en) * | 2009-07-15 | 2010-08-04 | 北京欣远诚业科技有限公司 | Flight illusion experience training simulator |
| CN101794524A (en) * | 2009-12-15 | 2010-08-04 | 中国民航大学 | Aircraft attitude-simulating 3-degree-of-freedom electrical turntable |
-
2010
- 2010-12-06 CN CN2010105752270A patent/CN102013188B/en not_active Expired - Fee Related
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101339701A (en) * | 2008-08-18 | 2009-01-07 | 吉林大学 | Three freedom degree movement simulation platform |
| CN201540661U (en) * | 2009-07-15 | 2010-08-04 | 北京欣远诚业科技有限公司 | Flight illusion experience training simulator |
| CN101794524A (en) * | 2009-12-15 | 2010-08-04 | 中国民航大学 | Aircraft attitude-simulating 3-degree-of-freedom electrical turntable |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104464441A (en) * | 2014-12-24 | 2015-03-25 | 喻明 | Flight simulation training device |
| 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 |
| CN111785126A (en) * | 2020-07-27 | 2020-10-16 | 中国工程物理研究院总体工程研究所 | Body rotation illusion simulation method integrating visual information and motion perception |
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| Publication number | Publication date |
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| CN102013188B (en) | 2012-07-18 |
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Granted publication date: 20120718 Termination date: 20121206 |