SDRE Guidance Law for Impact Angle Control against Moving Targets
In this paper,the terminal guidance problem of intercepting a moving target along a predetermined direction in the planar engagement scenario is considered.In this problem,two design specifications must be achieved: one is the minimum miss distance; and the other is the specified terminal impact angle.This problem is formulated as an infinite-horizon nonlinear regulator problem,and solved using the state-dependent Riccati equation (SDRE) method.To obtain a finite-horizon guidance law,a time-to-go based state weighting matrix is employed in the SDRE control scheme.In addition,to maintain the missile and the target in collision course and reduce the time-of-flight,the missile-target relative look angle is restricted using the SDRE control with a state constraint.Nonlinear simulations are performed to demonstrate the basic properties,applicability and robustness of the proposed guidance law.
State Dependent Riccati Equation Guidance Law Impact Angle Control Moving Target
QIAN Shaoke YANG Qiuhui ZHENG Zhiqiang
College of Mechatronics and Automation,National University of Defense Technology,Changsha,410073,P.R.China
国际会议
The 33th Chinese Control Conference第33届中国控制会议
南京
英文
831-836
2014-07-28（万方平台首次上网日期，不代表论文的发表时间）