A Design on Moving-Mass Actuated Reentry Vehicle with Predictive Guidance LaW
A new predictive guidance law for moving-mass actuated reentry vehicle is presented in this paper. The proposed approach is based on the fact that lateral force is formed in a plane which is perpendicular to the reentry vehicle velocity. Particularly, the nominal impact point is defined as the impact point generated by zero lift trajectory. The virtual displacement is defined as the tiny change of the nominal impact point, which is caused by any instantaneous lateral force at the beginning of the trajectory. The optimal direction of the lateral force is obtained by the solution of optimal virtual displacement, in which the optimal virtual displacement should point to the target. The linear quadratic gauss (LQG) method and the analytical solution of the reentry trajectory are used in this guidance method. Simulation results demonstrate the effectiveness of the proposed method.
Ruikang Li Wuxing Jing Changsheng Gao
Department of Aerospace Engineering,Harbin Institute of Technology,Harbin,15001,PR,China
国际会议
深圳
英文
920-924
2008-12-10（万方平台首次上网日期，不代表论文的发表时间）