This paper presents an application of adaptive control techniques to the design of skid-to-turn missile autopilot. The involved simplified adaptive controller is developed by combining gain scheduling approach with the eigenstructure assignment control design. A linear interpolation method is proposed to generate linear parameter-varying controller from a finite set of linear time-invariant controllers. Results of simulations are reported to demonstrate the performance, stability, and robustness of the considered autopilot.
Skid-to-turn missile autopilot design using scheduled eigenstructure assignment technique
2006-03-01
15 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Skid-to-turn missile autopilot design using scheduled eigenstructure assignment technique
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