Research on Inverse System Decoupling of Three-Axis Flight Simulator Based on the High-Speed Rotation Missile

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This paper researches on the kinematics and dynamics of coupling for three-axis flight Simulator based on the high-speed rotation missile. Firstly, to define station body coordinate and the positive direction of rotation according to three-axis flight Simulator based on the high-speed rotation missile, and then the mathematical coupling model is established. Secondly, multivariable nonlinear mathematical model can be decoupling, while substituting the parameters quality attribute analysis solved by ProE into the mathematical model. Lastly, the decoupled linear equations and the decoupling solutions based on inverse system method were given, and then to finish the simulation and to analysis the simulation results.

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Periodical:

Edited by:

Abdel Hamid Ismail Mourad

Pages:

323-328

Citation:

X. Y. Yan et al., "Research on Inverse System Decoupling of Three-Axis Flight Simulator Based on the High-Speed Rotation Missile", Applied Mechanics and Materials, Vol. 615, pp. 323-328, 2014

Online since:

August 2014

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* - Corresponding Author

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[2] Changyi Zhou. Trixie study design and control algorithms flight simulator control system [D] Chinese Academy of Science, 2005: 17.

[3] Qingshuang Zeng, Mao Wang , Shengcai Liu. Coupling and decoupling between the three-axis turntable frame kinetics[J]. Chinese Inertial Technology. 1997, 5(3): 44-49. -21.