导弹运动方程的逆解析解

针对在采用反馈线性化理论设计导弹飞行控制系统时控制器算法对导弹逆模型的要求 ,推导了导弹运动方程的逆解析解 ,包括导弹质心运动的运动学方程及其动力学方程的逆解析解、姿态运动的运动学方程及其动力学方程的逆解析解 ,详细给出了逆模型的求解过程 ,为一类飞行控制系统运用全局线性化设计奠定了基础。最后 ,结合工程应用进行了仿真计算 ,仿真结果表明逆解析解的推导是正确的

Inverse-analytic solution on motion equation of a missile

While designing a flight control system of a missile via feedback linearization, an inverse model of motion of a missile is required for the controller. In view of this situation, a set of inverse analytic solution of motion of a missile is inferred, which includes the dynamics and the kinematics equation of the center of mass and the attitude motion of a missile. A detail interring process is showed and a base is established for the design of a class of flight control system. The last, in the light of an engineering problem, a new flight control system is designed in reference1]. The simulation solution proves the inverse analytic solution correct.