A guidance law design using the combination of ISMC and SDRE schemes

Yew Wen Liang, Jun Yu Chen, Li Gang Lin

研究成果: 書貢獻/報告類型會議論文篇章同行評審

3 引文 斯高帕斯(Scopus)

摘要

This paper studies the design of a robust guidance law for missiles in the presence of uncertainties, which may include inaccurate prediction of target maneuver. Under the design, the closed-loop guidance system is shown to be robust to the uncertainties. Additionally, the scheme presented possesses the flexibility of allowing the engineer to select a desired guidance law for the nominal system (i.e., system without uncertainty) so that the state response of the overall uncertain guidance system is close to that of the selected nominal closed-loop guidance system. The simulation results demonstrate the benefits of the presented scheme.

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主出版物標題ICSSE 2013 - IEEE International Conference on System Science and Engineering, Proceedings
頁面63-67
頁數5
DOIs
出版狀態已出版 - 2013
事件IEEE International Conference on System Science and Engineering, ICSSE 2013 - Budapest, Hungary
持續時間: 4 7月 20136 7月 2013

出版系列

名字ICSSE 2013 - IEEE International Conference on System Science and Engineering, Proceedings

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???event.eventtypes.event.conference???IEEE International Conference on System Science and Engineering, ICSSE 2013
國家/地區Hungary
城市Budapest
期間4/07/136/07/13

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