Title :
H∞ guidance law with maneuvering targets
Author :
Yang, Ciann-Dong ; Chen, Hsin-Yuan
Author_Institution :
Inst. of Aeronaut. & Astronaut., Nat. Cheng Kung Univ., Tainan, Taiwan
Abstract :
In this paper we propose an H∞ robust guidance law for homing missiles with maneuvering targets. The nonlinear H∞ suboptimal control design governed by the Hamilton-Jacobi PDE inequality associated with this guidance problem is solved analytically. Based on the existing nonlinear H∞ techniques, we synthesize an H∞ guidance law which can pursue a class of maneuvering targets with acceptable energy consumption and miss distance
Keywords :
missile guidance; H∞ guidance law synthesis; H∞ robust guidance law; Hamilton-Jacobi PDE inequality; energy consumption; homing missiles; maneuvering targets; miss distance; nonlinear H∞ suboptimal control design; Attenuation; Control systems; Control theory; Differential equations; Ear; Jacobian matrices; Missiles; Navigation; Robustness; State feedback;
Conference_Titel :
Decision and Control, 1997., Proceedings of the 36th IEEE Conference on
Conference_Location :
San Diego, CA
Print_ISBN :
0-7803-4187-2
DOI :
10.1109/CDC.1997.657725
