Title :
Loop shaping design of a robust missile autopilot
Author :
White, B A ; Patel, Y. ; Vorley, D.H. ; Horton, M.
Author_Institution :
R. Mil. Coll. of Sci., Shrivenham, UK
Abstract :
An H∞ controller is designed for a latax autopilot missile, using the method of loop shaping and the central K algorithm of McFarlane and Glover (1989). The resulting autopilot is shown to have good robustness to variations in incidence and roll angle
Keywords :
H∞ control; control system synthesis; missile guidance; robust control; H∞ controller; central K algorithm; latax autopilot missile; loop shaping design; robust missile autopilot; robustness; Algorithm design and analysis; Centralized control; Closed loop systems; Instruments; Missiles; Open loop systems; Robust stability; Robustness; Shape control; Steady-state;
Conference_Titel :
American Control Conference, Proceedings of the 1995
Conference_Location :
Seattle, WA
Print_ISBN :
0-7803-2445-5
DOI :
10.1109/ACC.1995.529303
