DocumentCode
343084
Title
Naive control of the double integrator: a comparison of a dozen diverse controllers under off-nominal conditions
Author
Rao, Venkatesh G. ; Bernstein, Dennis S.
Author_Institution
Dept. of Aerosp. Eng., Michigan Univ., Ann Arbor, MI, USA
Volume
2
fYear
1999
fDate
2-4 Jun 1999
Firstpage
1477
Abstract
In naive control, a control algorithm derived under nominal, or ideal conditions is evaluated by analytical or numerical means under off-nominal, or non-ideal conditions that were not assumed in the formal synthesis procedure. Under such non-ideal conditions, the controller may or may not perform well. We consider an eclectic set of algorithms, ranging from classical to nonlinear and adaptive. Since the controllers are tuned by means of different procedures and since each controller has different capabilities, it is challenging to construct criteria that provide a useful evaluation of controller capabilities. Our approach to this problem is as follows. First, we specify nominal conditions in which the mass is given, and we tune each controller to minimize the worst case time to the origin from initial conditions located on the unit circle in the position/velocity phase plane without exceeding a peak input of unity. Next, we test each nominally tuned controller under a sequence of off nominal conditions
Keywords
closed loop systems; control system analysis; linear quadratic Gaussian control; linear systems; variable structure systems; closed loop systems; double integrator; linear quadratic Gaussian control; linear time invariant systems; naive control; nominal conditions; nonideal conditions; sliding mode control; tuning; Aerospace engineering; Algorithm design and analysis; Closed loop systems; Open loop systems; Output feedback; State feedback; Testing; Velocity control; Weight control;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1999. Proceedings of the 1999
Conference_Location
San Diego, CA
ISSN
0743-1619
Print_ISBN
0-7803-4990-3
Type
conf
DOI
10.1109/ACC.1999.783615
Filename
783615
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