DocumentCode
1751588
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
Volume
5
fYear
2001
fDate
2001
Firstpage
3352
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;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2001. Proceedings of the 2001
Conference_Location
Arlington, VA
ISSN
0743-1619
Print_ISBN
0-7803-6495-3
Type
conf
DOI
10.1109/ACC.2001.946146
Filename
946146
Link To Document