DocumentCode
1597976
Title
Missile endgame analysis
Author
Juang, Jyh-Ching ; Lin, Ching-Fang ; Evers, J.H. ; Cloutier, James R.
Author_Institution
American GNC Corp., Chatsworth, CA, USA
fYear
1992
Firstpage
744
Abstract
An endgame analysis and design framework are described. The framework can aid in understanding of the endgame dynamics, identifying critical design parameters, and bringing insights to the guidance/control design. A worst-case analysis approach is introduced and applied to the HAVE DASH II system. The analysis approach generalizes the covariance analysis method and provides a more accurate prediction of the engagement performance. On the basis of the analysis framework and performance measure, robust control design methods can be applied to obtain a robust integrated guidance and control design
Keywords
aerospace control; control system synthesis; missiles; navigation; HAVE DASH II system; aerospace control; covariance analysis; endgame analysis; endgame dynamics; guidance/control design; missiles; worst-case analysis; Acceleration; Aerodynamics; Equations; Missiles; Performance analysis; Pollution measurement; Random processes; Signal analysis; Stability; Virtual manufacturing;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Applications, 1992., First IEEE Conference on
Conference_Location
Dayton, OH
Print_ISBN
0-7803-0047-5
Type
conf
DOI
10.1109/CCA.1992.269754
Filename
269754
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