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