Title :
Advanced guidance law design based on the information-set concept
Author :
Emeliyanov, D. ; Rubinovich, E. ; Miller, B.
Author_Institution :
Inst. of Control Sci., Moscow, Russia
Abstract :
Addresses an approach to guidance algorithm design based on the concept of information sets (IS). As an example of guidance problemΓ a model of defense scenario against a reentering ballistic missile is considered. In this scenarioΓ a maneuverable decelerating target is to be destroyed by a hit-to-kill interceptor fitted with an IR array seeker and lateral impulse thrusters. The key element of the proposed approach is a description of the "interceptor-target" system state by means of IS. The results of Monte Carlo tests of the developed algorithm are presented
Keywords :
dynamics; extrapolation; missile guidance; set theory; IR array seeker; Monte Carlo tests; advanced guidance law design based; defense scenario; guidance problem; hit-to-kill interceptor; information-set concept; lateral impulse thrusters; maneuverable decelerating target; reentering ballistic missile; Additive noise; Algorithm design and analysis; Control system analysis; Drag; Force measurement; Missiles; Monte Carlo methods; Noise measurement; Optimal control; System testing;
Conference_Titel :
Decision and Control, 2001. Proceedings of the 40th IEEE Conference on
Conference_Location :
Orlando, FL
Print_ISBN :
0-7803-7061-9
DOI :
10.1109/.2001.980178
