Attitude Control and Vibration Suppression of the 1st Mode of Spacecraft with Flexible Structures Using Input Shaping

Autor:	Takashi Shimomura, Daiki Nakanishi, Sayaka Kanata
Rok vydání:	2020
Předmět:	Attitude control Vibration Spacecraft Computer science Control theory business.industry Input shaping Mode (statistics) business
Zdroj:	JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 68:148-155
ISSN:	2432-3691 1344-6460
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::63b91ea5d8356960201871cb796055f9 https://doi.org/10.2322/jjsass.68.148 Zobrazit plný text záznamu