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

Xin Ying Yan; Bo Mo; Yang Hua Li

doi:10.4028/www.scientific.net/AMM.615.323

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 615Research on Inverse System Decoupling of...

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

Abstract:

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:

Applied Mechanics and Materials (Volume 615)

Pages:

323-328

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.615.323

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Online since:

August 2014

Authors:

Xin Ying Yan*, Bo Mo, Yang Hua Li

Keywords:

Decoupling, High-Speed Rotation Missile, Inverse System, Three-Axis Flight Simulator

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* - Corresponding Author

References

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