DocumentCode :
2339019
Title :
Minimum energy guidance for boost phase ballistic missile interception
Author :
Guelman, M. ; Golan, O.M.
Author_Institution :
Technion-Israel Inst. of Technol., Haifa, Israel
Volume :
6
fYear :
1995
fDate :
21-23 Jun 1995
Firstpage :
4131
Abstract :
Using as the optimality index the required energy for interception of a ballistic missile in its boost phase, it is shown that the cost has an absolute minimum for a finite interception duration. The problem of interception of a thrusting target has an optimal solution for a free final time. The required interceptor three dimensional acceleration vector for the interception of a ballistic missile in its boost phase is derived in feedback form. Time to go, the critical variable in all optimal guidance laws, is derived in closed form as the solution of a nonlinear algebraic equation. Closed loop implementation of the optimal guidance law is based on the current prediction of the target trajectory. Numerical results for a representative intercept are presented
Keywords :
feedback; minimum principle; missile guidance; ballistic missile; boost phase ballistic missile interception; closed loop implementation; feedback; finite interception duration; interceptor three dimensional acceleration vector; minimum energy guidance; nonlinear algebraic equation; optimal guidance laws; optimality index; target trajectory prediction; thrusting target; Acceleration; Aircraft; Cost function; Feedback; Missiles; Nonlinear equations; Optimal control; Trajectory; Vectors; Velocity control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, Proceedings of the 1995
Conference_Location :
Seattle, WA
Print_ISBN :
0-7803-2445-5
Type :
conf
DOI :
10.1109/ACC.1995.532709
Filename :
532709
Link To Document :
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