Research on Inverse System Decoupling of Three-Axis Flight Simulator Based on the High-Speed Rotation Missile
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.
Abdel Hamid Ismail Mourad
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