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
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;
Conference_Titel :
Control Applications, 1992., First IEEE Conference on
Conference_Location :
Dayton, OH
Print_ISBN :
0-7803-0047-5
DOI :
10.1109/CCA.1992.269754