Guidance law against maneuvering targets with intercept angle constraint.

Xiong, Shaofeng; Wang, Weihong; Liu, Xiaodong; Wang, Sen; Chen, Zengqiang

Xiong, Shaofeng; Wang, Weihong; Liu, Xiaodong; Wang, Sen; Chen, Zengqiang.

Afiliación

Xiong S; School of Automation Science and Electrical Engineering, Beijing University of Aeronautics & Astronautics, Beijing 100191, China; Science and Technology on Aircraft Control Laboratory, Beijing University of Aeronautics & Astronautics, Beijing 100191, China. Electronic address: 15210985746@16
Wang W; School of Automation Science and Electrical Engineering, Beijing University of Aeronautics & Astronautics, Beijing 100191, China; Science and Technology on Aircraft Control Laboratory, Beijing University of Aeronautics & Astronautics, Beijing 100191, China.
Liu X; Beijing Aerospace Automatic Control Institute, Beijing 100854, China; National Key Laboratory of Science and Technology on Aerospace Intelligence Control, Beijing 100854, China.
Wang S; School of Automation Science and Electrical Engineering, Beijing University of Aeronautics & Astronautics, Beijing 100191, China; Science and Technology on Aircraft Control Laboratory, Beijing University of Aeronautics & Astronautics, Beijing 100191, China.
Chen Z; Department of Automation, Nankai University, Tianjin 300071, China.

ISA Trans ; 53(4): 1332-42, 2014 Jul.

Article en En | MEDLINE | ID: mdl-24773919

Palabras clave

Extended state observer; Intercept angle constraint; Maneuvering target; Nonlinear guidance law; Sliding mode control

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Texto completo: 1 Colección: 01-internacional Base de datos: MEDLINE Tipo de estudio: Guideline Idioma: En Revista: ISA Trans Año: 2014 Tipo del documento: Article