Minimum-Effort Impact-Time Control Guidance Using Quadratic Kinematics Approximation

被引:12
|
作者
Merkulov, Gleb [1 ]
Weiss, Martin [1 ]
Shima, Tal [1 ]
机构
[1] Technion Israel Inst Technol, Fac Aerosp Engn, IL-3200003 Haifa, Israel
关键词
Kinematics Approximation; Control Guidance; Transversality Condition; Numerical Optimization; Sensors; Numerical Simulation; Autopilot; Closed Loop; Shape Functions; Brute Force Search; EFFORT INTERCEPT; LAW; ANGLE; ALGORITHMS;
D O I
10.2514/1.G006190
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A guidance law for intercepting a stationary target is derived based on solving the minimum effort optimal control problem with fixed terminal time and a quadratic approximation of the kinematic equations. It is proven that this optimal control problem has, in general, a unique solution. Based on this solution, a guidance law is proposed that is shown to be implementable based on typically available sensor data, using a semi-analytic procedure. Numerical simulations show that the solution based on the quadratic kinematics approximation matches closely the solution based on the original nonlinear kinematics that can only be obtained by numerical optimization.
引用
收藏
页码:348 / 361
页数:14
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