Title :
Robust state dependent Riccati equation based guidance laws
Author :
Balakrishnan, Sivasubramanya N. ; Xin, Ming
Author_Institution :
Dept. of Mech. & Aerosp. Eng., Missouri Univ., Rolla, MO, USA
Abstract :
A robust state dependent Riccati equation based guidance/control is investigated in this study. In order to have a better design tool in terms of required interceptor accelerations, the target intercept geometry is formulated in a set of polar coordinates. With this formulation, we formulate a cost function with state dependent weights. In this study, we investigate the effects of such cost functions on the levels of interceptor accelerations. We also synthesize a neural network based extra controller to achieve the robustness in the presence of the target acceleration. In this manner, we will not need target acceleration estimation explicitly in the guidance law
Keywords :
Riccati equations; control system synthesis; missile guidance; neurocontrollers; robust control; cost function; homing missile guidance; intercept geometry; interceptor accelerations; missile control; neural network based extra controller; polar coordinates; robust state dependent Riccati equation based guidance laws; state dependent weights; Acceleration; Cost function; Missiles; Navigation; Nonlinear equations; Optimal control; Riccati equations; Robust control; Robustness; Sliding mode control;
Conference_Titel :
American Control Conference, 2001. Proceedings of the 2001
Conference_Location :
Arlington, VA
Print_ISBN :
0-7803-6495-3
DOI :
10.1109/ACC.2001.946146