Modeling and Analysis of Micro-Spacecraft Attitude Sensing with Gyrowheel.

Liu, Xiaokun; Zhao, Hui; Yao, Yu; He, Fenghua

Liu, Xiaokun; Zhao, Hui; Yao, Yu; He, Fenghua.

Afiliação

Liu X; School of Astronautics, Harbin Institute of Technology, No. 2 Yikuang Street, Nangang District, Harbin 150080, China. hitlxk@gmail.com.
Zhao H; School of Astronautics, Harbin Institute of Technology, No. 2 Yikuang Street, Nangang District, Harbin 150080, China. zhaohui@hit.edu.cn.
Yao Y; School of Astronautics, Harbin Institute of Technology, No. 2 Yikuang Street, Nangang District, Harbin 150080, China. yaoyu@hit.edu.cn.
He F; School of Astronautics, Harbin Institute of Technology, No. 2 Yikuang Street, Nangang District, Harbin 150080, China. hefenghua@hit.edu.cn.

Sensors (Basel) ; 16(8)2016 Aug 19.

Article em En | MEDLINE | ID: mdl-27548178

Palavras-chave

complex quantity; dynamic measurement; gyrowheel; micro-spacecraft angular rate sensing; real-time Lyapunov linearization; static measurement

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Texto completo: 1 Coleções: 01-internacional Base de dados: MEDLINE Tipo de estudo: Prognostic_studies Idioma: En Revista: Sensors (Basel) Ano de publicação: 2016 Tipo de documento: Article

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