NDLI: Integrated Estimation, Guidance, and Control System Design Using Game Theoretic Approach

Content Provider	IEEE Xplore Digital Library
Author	Lin, C. F. Wang, Q. Spayer, Jason L. Evers, Johy H. Cloutier, James R.
Copyright Year	1992
Description	Author affiliation: American GNC Corporation, 9131 Mason Avenue, Chatsworth, California 91311, USA (Lin, C. F.; Wang, Q.) \|\| Department of Mechanical Aerospace and Nuclear Engineering, University of California, Los Angeles California 90024, USA (Spayer, Jason L.) \|\| USAF Armament Directorate of Wright Laboratory, WL/MNAG Eglin AFB, Florida 32542, USA (Evers, Johy H.; Cloutier, James R.)
Abstract	In order to produce a robust coupling between the guidance system and autopilot and improve the target intercept capability, the game theoretic approach is applied to the derivation of an integrated estimation, guidance and control scheme for missile intercept problem. The objective of fomulating the game problem is to find a contoller, combining the guidance law and autopilot controller, which minimizes the final miss distance and the control energy in the worst case of target maneuver and the worst case of measurement uncertainty, and to find an estimator that provides feedback information for autopilot implementation and target tracking information for guidance processing. The controller and estimator obtained from the game theoretic approach form a linear n-dimensional compensator and the controller is solved in closed-form. In a full information and nonmaneuver case, the solution recovers the integrated guidance and control (IGC) law designed by using the linear quadratic optimal approach as presented in [Lin and Yueh, 1984(a)-(c); Yueh and Lin, 1985].
Starting Page	3220
Ending Page	3224
File Size	453460
Page Count	5
File Format	PDF
ISBN	0780302109
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	1992-06-24
Publisher Place	USA
Access Restriction	Subscribed
Rights Holder	American Automatic Control Council(AACC)
Subject Keyword	Control systems Game theory Optimal control Linear feedback control systems State estimation Missiles Error correction Robust control Uncertainty Aerodynamics
Content Type	Text
Resource Type	Article

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