DocumentCode
335427
Title
Control of a bank-to-turn (BTT) missile with saturating actuators
Author
Rodriguez, Armando A. ; Cloutier, James R.
Author_Institution
Dept. of Electr. Eng., Arizona State Univ., Tempe, AZ, USA
Volume
2
fYear
1994
fDate
29 June-1 July 1994
Firstpage
1660
Abstract
In this paper, a method is presented for enhancing the performance of a stable EMRAAT bank-to-turn (BTT) missile in the presence of multiple saturating actuators. The method involves the design of a saturation detection system, called an error governor which maintains, to the extent possible, the multivariable properties of the original autopilot design. The system prevents saturation, ensures finite-gain L∞ stability, and maintains, to the extent possible, the directionality properties of the original autopilot.
Keywords
actuators; error compensation; feedback; missile control; multivariable control systems; stability; EMRAAT missile; autopilot; bank-to-turn missile; compensator; directionality; error governor; finite-gain L∞ stability; multivariable feedback; saturating actuators; saturation detection system; Actuators; Control systems; Design methodology; Differential equations; Error correction; Feedback loop; MIMO; Missiles; Stability; Systems engineering and theory;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1994
Print_ISBN
0-7803-1783-1
Type
conf
DOI
10.1109/ACC.1994.752353
Filename
752353
Link To Document