Design and Analysis of Sustained-G Flight Simulator Control Algorithm

doi:10.16182/j.issn1004731x.joss.17-0303

Abstract

Abstract: In order to solve the problem of mismatch exist between angular motions by Sustained-G Flight Simulator pilot through his proprioceptive receptors and visual receptors, the control algorithm of Sustained-G Flight Simulator is designed. The formulas relative to control input is derived; the mathematical model of human proprioceptive system is researched, the relationship between pilot's perceptual angular and rotating linear acceleration vectors and angular accelerations is given, based on that, the control algorithm of Sustained-G Flight Simulator is proposed, which can make a match existence between the angular motion perceived by Sustained-G Flight Simulator pilot and aircraft pilot. The simulation results show that the control algorithm presented can effectively solve the problem of mismathching existence between angular motions by Sustained-G Flight Simulator pilot through his proprioceptive receptors and visual receptors, and improve the flight realism of Sustained-G Flight Simulator.

Key words: Sustained-G Flight Simulator, human proprioceptive system, acceleration, angular motion

CLC Number:

TP391.9

Zhou Xiaoguang, Fang Yihong, Tian Huaiying, Yao Mingzhi. Design and Analysis of Sustained-G Flight Simulator Control Algorithm[J]. Journal of System Simulation, 2019, 31(9): 1835-1841.

References

[1] 潘文俊, 王立新. 持续载荷飞行模拟器过失速机动过载模拟[J]. 北京航空航天大学学报, 2011, 37(6): 635-640.
Pan Wenjun, Wang Lixin.Simulation of G-Ioads in post-stall maneuver on sustained G-Ioad flight simulaton[J]. Joumal of Beijing University of Aeronautics and Astronautics, 2011, 37(6): 635-640.
[2] 潘文俊, 王立新. 持续载荷飞行模拟器过载模拟新原理[J]. 航空学报, 2010, 31(11): 2160-2166.
Pan Wenjun, Wang Lixin.Principles of G-load simulation for novel Sustained-G Flight Simulation[J]. Acta Aeronautica Astronautica Sinica, 2010, 31(11): 2160-2166.
[3] 由俊生, 由勇. 歼击机飞行员三轴加速度过载建模与仿真研究[J]. 系统仿真学报, 2006, 18(增2): 28-30.
You Junsheng, You Yong.Research for modelling and simulation of pilot three shaft acceleration[J]. Journal of System Simulation, 2006, 18(S2): 28-30.
[4] 由勇, 由育阳. 持续载荷飞行仿真技术与工程设计[M]. 北京: 国防工业出版社, 2013.
You Yong, You Yuyang.Sustained Acceleration Flight Simulation Technology And Engineering Design[M]. Beijing: National Defence of Industry Press, 2013.
[5] 宋琼, 胡荣华. 动态飞行模拟器及其发展概述[J]. 装备环境工程, 2015, 12(5): 11-16.
Song Qiong, Hu Ronghua.Summarization of Dynamic Flight Simulator and Its Development[J]. Equipment Enviroment Engineering, 2015, 12(5): 11-16.
[6] Crobie R J, Kiefer D A.Controlling the human centrifuge as a force and motion platform for the dynamic flight simulator[R]. AIAA-1985-1742, 1985.
[7] Tripathy N K.Analysis of multiaxis acceleration profile in a supermaneuverable aircraft[J]. Indian Journal of Aerospace Medicine (S0884-2914), 2006, 50(2): 7-12.
[8] Richard J C.Application of experimental derived pilot perceptual angular response transfer function[R]. AIAA-1988-1100, 1988: 146-153.
[9] Repperger D W.A study of supermaneuverable flight trajectories through motion field simulation of centrifuge simulation[J]. Journal of Dynamic Systems, Measurement and Control (S0022-0434), 1992, 270(114): 556-560.
[10] Crosbie R J.A total G-force environment dynamic flight simulator[R]. AIAA-83-0139, 1983.
[11] Dennis K.Development evaluation of a centrifuge flight simulator as an enhance maneuverability flying qualities tool[R]. AIAA-92-4157-CP, 1992.
[12] Rogers R O.An Experiment to Evaluate Transfer of Low-Cost Simulator-Based Upset-Recovery Training[R]. AIAA-09-5257-CP, 2009.
[13] Antonio O.New concept of dynamic flight simulator[J]. Aerospace Science and Technology (S1207-9638), 2013, 126(30): 79-80.
[14] Richard M M.A Study to Evaluate the Suitability of a Centrifuge as a Dynamic Flight Simulator for F/A-18 Strike Fighter Mission Training[D]. Knoxville: University of Tennessee, 2009.