DocumentCode
313830
Title
High performance bounded control
Author
Shewchun, J. Marc ; Feron, Eric
Author_Institution
Dept. of Aeronaut. & Astronaut., MIT, Cambridge, MA, USA
Volume
5
fYear
1997
fDate
4-6 Jun 1997
Firstpage
3250
Abstract
The high performance bounded (HPB) control methodology is based upon the idea of using progressively higher gains as the system approaches equilibrium to avoid actuator saturation and to improve performance. In this paper three new theoretical results are presented. The first provides a formal stability proof for the HPB control scheme. The second provides a method for dealing with asymmetric position constraints. The third allows for the incorporation of actuator rate constraints into the HPB methodology
Keywords
stability; HPB control; actuator rate constraints; actuator saturation; asymmetric position constraints; high-performance bounded control; stability; Actuators; Aerodynamics; Control systems; Ellipsoids; Lyapunov method; Performance gain; Riccati equations; Space technology; Stability; Strain control;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1997. Proceedings of the 1997
Conference_Location
Albuquerque, NM
ISSN
0743-1619
Print_ISBN
0-7803-3832-4
Type
conf
DOI
10.1109/ACC.1997.612061
Filename
612061
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