Problem of precision missile guidance: LQR and H//infin// control frameworks

Addressed here is the precision missile guidance problem where the successful intercept criterion has been defined in terms of both minimizing the miss distance and controlling the missile body attitude with respect to the target at the terminal point. We show that the H//infin// control theory, whe...

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Veröffentlicht in:	IEEE transactions on aerospace and electronic systems 2003-07, Vol.39 (3), p.901-910
Hauptverfasser:	Savkin, A V, Pathirana, P N, Faruqi, F A
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Sprache:	eng
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creator	Savkin, A V Pathirana, P N Faruqi, F A
description	Addressed here is the precision missile guidance problem where the successful intercept criterion has been defined in terms of both minimizing the miss distance and controlling the missile body attitude with respect to the target at the terminal point. We show that the H//infin// control theory, when suitably modified, provides an effective framework for the precision missile guidance problem. The existence of feedback controllers (guidance laws) is investigated for the case of finite horizon and non-zero initial conditions. Both state feedback and output feedback implementations are explored.
doi_str_mv	10.1109/TAES.2003.1238744
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title	Problem of precision missile guidance: LQR and H//infin// control frameworks
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