Impact angle constrained three-dimensional integrated guidance and control for STT missile in the presence of input saturation.

Wang, Sen; Wang, Weihong; Xiong, Shaofeng

Wang, Sen; Wang, Weihong; Xiong, Shaofeng.

Afiliación

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. Electronic address: wangsenxiaoya@163.com.
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.
Xiong S; Beijing Institute of Space Launch Technology, Beijing 100076, China.

ISA Trans ; 64: 151-160, 2016 Sep.

Article en En | MEDLINE | ID: mdl-27167987

Palabras clave

Constrained terminal impact angle; Dynamic surface control; Integrated guidance and control; Nussbaum function; Saturation

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Texto completo: 1 Banco de datos: MEDLINE Tipo de estudio: Guideline / Prognostic_studies Idioma: En Revista: ISA Trans Año: 2016 Tipo del documento: Article

Texto completo

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PubMed Links

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Texto completo: 1 Banco de datos: MEDLINE Tipo de estudio: Guideline / Prognostic_studies Idioma: En Revista: ISA Trans Año: 2016 Tipo del documento: Article