https://scholars.lib.ntu.edu.tw/handle/123456789/150143
標題: | A nonlinear constant bearing guidance and adaptive autopilot design for BTT missiles | 作者: | LI-CHEN FU Chang, Wei-Der Chuang, Dung-Ming Kuo, Te-Son Wang, Tze-Chien Tsai, Chi-Wang |
公開日期: | 六月-1997 | 卷: | 5 | 起(迄)頁: | 2774 - 2778 | 來源出版物: | Proceedings of the American Control Conference | 會議論文: | Proceedings of the 1997 American Control Conference. Part 3 (of 6) | 摘要: | This paper is an integration of two earlier results on missile guidance and autopilot. The guidance design is a nonlinear implementation of the constant bearing guidance. The guidance command in the form of acceleration is transformed into acceptable forms for the autopilot design. This design incorporates feedforward neural networks in the structure of adaptive control. Its weighting matrices and other unknown parameters are tuned on-line, and the approximation error of the neural networks is compensated via the technique of sliding mode control. Stability and performance for the integrated system are also investigated. |
URI: | http://ntur.lib.ntu.edu.tw//handle/246246/2007041910031864 https://www.scopus.com/inward/record.uri?eid=2-s2.0-0030652284&partnerID=40&md5=88a8d87d6eaf6d603b6e1e664ab66004 |
ISSN: | 07431619 | 其他識別: | N/A | DOI: | 10.1109/ACC.1997.611960 | SDG/關鍵字: | Adaptive control systems; Approximation theory; Control system analysis; Error compensation; Feedforward neural networks; Missiles; Nonlinear control systems; System stability; Bank to turn missiles; Missile autopilot; Nonlinear constant bearing guidance; Electronic guidance systems |
顯示於: | 電機工程學系 |
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