A re-entry guidance method for vehicle using virtual displacement concept

C. Gao, Ruikang Li, W. Jing
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引用次数: 1

Abstract

A new guidance law for 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 analytical solution of reentry trajectory and the linear quadratic gauss (LQG) method are used to design this guidance law. The simulation results demonstrate the effectiveness of the proposed method
基于虚拟位移概念的飞行器再入制导方法
提出了一种新的再入飞行器制导律。提出的方法是基于侧向力在垂直于再入飞行器速度的平面上形成的事实。其中,标称冲击点定义为零升力轨迹产生的冲击点。虚拟位移被定义为标称撞击点的微小变化,这是由轨迹开始时的任何瞬时侧向力引起的。通过求解最优虚位移得到横向力的最优方向,其中最优虚位移应指向目标。采用再入弹道解析解和线性二次高斯(LQG)方法设计了该制导律。仿真结果验证了该方法的有效性
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