Title :
Optimal guidance for high order maneuvering target and high order missile
Keywords :
Acceleration; Differential equations; Estimation theory; Missiles; Nonlinear filters; Optimal control; Performance analysis; Riccati equations; State estimation; Transfer functions;
Conference_Titel :
Control and Applications, 1989. Proceedings. ICCON '89. IEEE International Conference on
DOI :
10.1109/ICCON.1989.770497
