DocumentCode :
3402497
Title :
Second and third order minimum time controllers and missile adjoints
Author :
Titus, H. ; Cooper, C.R.
Author_Institution :
US Naval Postgraduate Sch., Monterey, CA, USA
fYear :
1991
fDate :
14-17 May 1991
Firstpage :
482
Abstract :
The optimal minimum time control (i.e. a bang-bang controller) is applied to the fast reaction missile defense problem. The control may be posed either as a function of time or as a function of the states. The state space can be partitioned into regions, surfaces, and curves where the optimal control action is either its maximum plus or minus N. In missile simulation problems, the method of adjoints is often used in parametric studies of errors and miss distance. This technique is used to help visualize the solution trajectory and families of optimal trajectories for all possible initial conditions
Keywords :
bang-bang control; missiles; optimal control; bang-bang controller; families of optimal trajectories; fast reaction missile defense problem; initial conditions; minimum time controllers; miss distance; missile adjoints; missile simulation problems; optimal control action; parametric studies; second-order controllers; solution trajectory; third-order controllers; Boundary value problems; Control systems; Equations; Error correction; Missiles; Optimal control; Parametric study; State-space methods; USA Councils; Visualization;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Circuits and Systems, 1991., Proceedings of the 34th Midwest Symposium on
Conference_Location :
Monterey, CA
Print_ISBN :
0-7803-0620-1
Type :
conf
DOI :
10.1109/MWSCAS.1991.252200
Filename :
252200
Link To Document :
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