A flight simulator side-by-side driving control linkage and loading device
A flight simulator and driving control technology, applied in the field of flight simulation, can solve problems such as poor reliability of the structure, uncontrollable loading effect, device simulation sampling, etc., and achieve the effect of reducing connection links, optimal component form, and strong real-time performance
Active Publication Date: 2019-08-30
SHANGHAI UNIV OF ENG SCI
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Problems solved by technology
[0003] The invention provides a flight simulator seat-by-seat driving control linkage and loading device, which solves the problems of the existing device, such as rough simulation sampling, sluggish control response, uncontrollable loading effect, and poor structural reliability.
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[0019] The specific implementation manner of the present invention will be described in detail below in conjunction with the accompanying drawings and preferred embodiments.
[0020] At present, the side-by-seat structure of flight simulation driving control mostly appears in the simulation of large aircraft. There are various methods to realize the simulation, but this type of structure must ensure the composite function of longitudinal push-pull and horizontal turntable at the same time, in terms of mechanism transmission accuracy and The standard for eliminating component motion interference is relatively high, so many similar system structures are very complex, and there is still no optimal solution that can take into account "system optimization" and "function realization".
[0021] The present invention provides a flight simulator side-by-side driving control interlocking and loading device, comprising main and co-pilot control panels 1 and 14, a horizontal linkage mechan...
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The invention belongs to the technical field of flight simulation, and discloses a flight simulator side-by-side drive maneuvering linkage and loading device. The device comprises primary and secondary drive maneuvering panels, a horizontal linkage mechanism, a longitudinal linkage mechanism, a horizontal loading mechanism connected with the horizontal linkage mechanism and a longitudinal loading mechanism connected with the longitudinal linkage mechanism, wherein the horizontal linkage mechanism and the longitudinal linkage mechanism are connected with the primary and secondary drive maneuvering panels. The horizontal linkage mechanism is used for realizing the linkage of the horizontal maneuvering between the primary and secondary drive maneuvering panels. The longitudinal linkage mechanism is used for realizing the linkage of the longitudinal maneuvering between the primary and secondary drive maneuvering panels. The horizontal loading mechanism is used for detecting the angular displacement of the horizontal maneuvering between the primary and secondary drive maneuvering panels to load a force based on the detected angular displacement. The longitudinal loading mechanism is used for detecting the angular displacement of the longitudinal maneuvering between the primary and secondary drive maneuvering panels to load a force based on the detected angular displacement. The flight simulator side-by-side drive maneuvering linkage and loading device provided by the invention has the advantages of concise structure, reasonable design, strong real-time performance, direct human-computer interaction and realistic simulation.
Description
technical field [0001] The invention belongs to the technical field of flight simulation, and in particular relates to a flight simulator side-by-side driving control linkage and loading device. Background technique [0002] The flight simulator is a special equipment for pilots to carry out training. The driving control linkage and loading mechanism system is a key subsystem in the flight simulator, and its performance directly affects the level of flight training. According to the different types and models of side-by-side aircraft, it is necessary to provide corresponding side-by-side driving control linkage and loading mechanism to simulate the driving control effect and training environment. With the development of the domestic aviation industry, the level of demand for flight simulators is gradually increasing, and there is an urgent need to develop a linkage loading control mechanism with the same level of standardization. At present, there are few analyzes and desig...
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IPC IPC(8): G09B9/04
Inventor 史健勇陈曦谢东来何法江王铮司华伟李宏图马天楚钟鸣王大勇贾慈力隋成城蒋龙威谢晨李程曹达敏
Owner SHANGHAI UNIV OF ENG SCI