Control Design for a Critical LEO Earth Observation Satellite, Based on GNSS Sensors for Orbit and Attitude Determination

Control Design for a Critical LEO Earth Observation Satellite, Based on GNSS Sensors for Orbit and Attitude Determination

著者名:

Llorente, J.S. ( SENER Ingenieria y Sistemas, S.A., Spain )

Fernandez-Ibarz, I.M. ( SENER Ingenieria y Sistemas, S.A., Spain )

Del Cura, J.M. ( SENER Ingenieria y Sistemas, S.A., Spain )

Marco, V ( SENER Ingenieria y Sistemas, S.A., Spain )

Casado, J.L. ( SENER Ingenieria y Sistemas, S.A., Spain )

Fuchs, J ( ESA ESTEC, The Netherlands )

さらに 1 件

掲載資料名:

4th ESA International Conference on Spacecraft Guidance, Navigation, and Control Systems : and tutorial on modern and robust control, theory, tools and applications, 18-21 October 1999, ESTEC, Noordwijk, The Netherlands

シリーズ名:

ESA SP

シリーズ巻号:

425

発行年:

2000

開始ページ:

153

終了ページ:

160

総ページ数:

8

出版情報:

Noordwijk, Netherlands: ESA Publications Division

ISSN:

03796566

ISBN:

9789290927006 [9290927003]

言語:

英語

請求記号:

E11690/425

資料種別:

国際会議録

詳細

TDL書誌ID:	ZA00013432
シリーズID:	PA00000009
会議名:	ESA International Conference on Spacecraft Guidance, Navigation, and Control Systems
回次:	4th
会議開催地:	Noordwijk, The Netherlands
会議開催年:	1999.10.18-1999.10.21

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