DocumentCode
3466938
Title
Blended aero and reaction jet missile autopilot design using VSS techniques
Author
Weil, Roark D. ; Wise, Kevin A.
Author_Institution
McDonnell Douglas Missile System Co., St. Louis, MO, USA
fYear
1991
fDate
11-13 Dec 1991
Firstpage
2828
Abstract
The use of variable structured system (VSS) control techniques to design the longitudinal autopilot for a missile under combined aerodynamic surface (fin) and reaction jet control is discussed. High-gain feedback employing singular perturbation analysis is used to design the reaction jet switching surfaces and the fin control law. The work extends work in which all controls were assumed to be linear or bang-bang but not blended
Keywords
bang-bang control; control system synthesis; feedback; linear systems; missiles; perturbation techniques; variable structure systems; aerodynamic surface; bang-bang; blended control; control system synthesis; fin control law; high gain feedback; linear; longitudinal autopilot; missile; reaction jet control; singular perturbation analysis; variable structured system; Aerodynamics; Control systems; Eigenvalues and eigenfunctions; Equations; Feedback; H infinity control; History; Missiles; Motion control; Performance gain; Sliding mode control; Variable structure systems;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1991., Proceedings of the 30th IEEE Conference on
Conference_Location
Brighton
Print_ISBN
0-7803-0450-0
Type
conf
DOI
10.1109/CDC.1991.261051
Filename
261051
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