DocumentCode :
3334646
Title :
Understanding missile autopilot design using the H loop shaping design procedure
Author :
Urban, Thomas J. ; Iwaskiw, Pete ; Iglesias, Pablo A.
Author_Institution :
Appl. Phys. Lab., Johns Hopkins Univ., Laurel, MD, USA
Volume :
1
fYear :
1999
fDate :
1999
Firstpage :
236
Abstract :
This paper presents different controller topologies for a missile autopilot. The controllers are based on a loop shaping design procedure due to McFarlane and Glover. The nature of the controllers obtained is discussed and a novel procedure for the selection of weights is given
Keywords :
H control; closed loop systems; control system synthesis; missile control; H loop shaping design procedure; controller topologies; missile autopilot design; weight selection; Acceleration; Control design; Feedback loop; Missiles; Open loop systems; Robust control; Robustness; Shape control; Topology; Tracking loops;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Applications, 1999. Proceedings of the 1999 IEEE International Conference on
Conference_Location :
Kohala Coast, HI
Print_ISBN :
0-7803-5446-X
Type :
conf
DOI :
10.1109/CCA.1999.806205
Filename :
806205
Link To Document :
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