Problem of precision missile guidance: LQR and H[infon] 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(infiniti) control theory whe...
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| Veröffentlicht in: | IEEE transactions on aerospace and electronic systems 2003-07, Vol.39 (3), p.901-910 |
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| container_title | IEEE transactions on aerospace and electronic systems |
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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(infiniti) control theory when suitably modified provides an effective framework for the precision missile guidance problem. 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. (Author) |
| doi_str_mv | 10.1109/TAES.2003.1238744 |
| format | Article |
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We show that the H(infiniti) control theory when suitably modified provides an effective framework for the precision missile guidance problem. 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. (Author)</description><identifier>ISSN: 0018-9251</identifier><identifier>EISSN: 1557-9603</identifier><identifier>DOI: 10.1109/TAES.2003.1238744</identifier><language>eng</language><publisher>New York: The Institute of Electrical and Electronics Engineers, Inc. (IEEE)</publisher><ispartof>IEEE transactions on aerospace and electronic systems, 2003-07, Vol.39 (3), p.901-910</ispartof><rights>Copyright The Institute of Electrical and Electronics Engineers, Inc. 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| language | eng |
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| title | Problem of precision missile guidance: LQR and H[infon] control frameworks |
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