DocumentCode
1537764
Title
Naive control of the double integrator
Author
Rao, Venkatesh G. ; Bernstein, Dennis S.
Author_Institution
Dept. of Aerosp. Eng., Michigan Univ., Ann Arbor, MI, USA
Volume
21
Issue
5
fYear
2001
fDate
10/1/2001 12:00:00 AM
Firstpage
86
Lastpage
97
Abstract
We deal with a form of controller evaluation that may be called naive control. In naive control, a control algorithm derived under nominal (or ideal) conditions is evaluated by analytical or numerical means under off-nominal (or nonideal) conditions that were not assumed in the formal synthesis procedure. Under such nonideal conditions, the controller may or may not perform well. This approach is distinct from robust control, which seeks to accommodate off-nominal perturbations in the synthesis procedure. We consider the double integrator plant, which is one of the most fundamental systems in control applications, representing single degree-of-freedom translational and rotational motion. Applications of the double integrator include low-friction, free rigid-body motion, such as single-axis spacecraft rotation and rotary crane motion. The double integrator plant considered includes a saturation nonlinearity on the control input
Keywords
control nonlinearities; control system synthesis; cranes; nonlinear control systems; optimal control; space vehicles; stability; control nonlinearity; control synthesis; double integrator; naive control; nonideal conditions; nonlinear control systems; rotary crane; spacecraft; Adaptive control; Control system synthesis; Control systems; Cranes; Motion control; Programmable control; Sliding mode control; Space vehicles; Testing; Velocity control;
fLanguage
English
Journal_Title
Control Systems, IEEE
Publisher
ieee
ISSN
1066-033X
Type
jour
DOI
10.1109/37.954521
Filename
954521
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