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

Volume

1

fYear

2001

fDate

2001

Firstpage

652

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;

fLanguage

English

Publisher

ieee

Conference_Titel

Decision and Control, 2001. Proceedings of the 40th IEEE Conference on

Conference_Location

Orlando, FL

Print_ISBN

0-7803-7061-9

Type

conf

DOI

10.1109/.2001.980178

Filename

980178