Design and Development of the Small Satellite Attitude Control System Simulator

Design and Development of the Small Satellite Attitude Control System Simulator

著者名:

Y. Yang ( Harbin Institute of Technology, Harbin, China (prc) )
X. Cao

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA Modeling and Simulation Technologies Conference

シリーズ巻号:

2006

発行年:

2006

通号:

2006-6124

ペーパー番号:

AIAA Paper 2006-6124

出版情報:

Reston, Va: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200620 [CD-ROM 2006 Disc 20]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00047248
シリーズID:	PA00000166
会議名:	AIAA Modeling and Simulation Technologies Conference and Exhibit
回次:	2006
会議開催地:	Keystone, Colorado
会議開催年:	2006.08.21-2006.08.24

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1 テクニカルペーパー Small Satellite Large Angle Attitude Maneuver Hardware-in-the-Loop Simulation Based on Three-axis Air Bearing Table F. Wang, X. Cao, Y. Yang, D. Gao American Institute of Aeronautics and Astronautics	7 テクニカルペーパー "Integrated Orbit, Attitude, and Structural Control System Design for Space Solar Power Satellites" Wie,B., Roithmayr,C. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー DESIGN OF A SPHERICAL AIR BEARING SIMULATOR FOR TESTS OF THE ATTITUDE CONTROL SYSTEM OF ARTIFICIAL SATELLITES Cardieri, Luiz Victor C. et al. National Aeronautics and Space Administration	8 テクニカルペーパー SIMULATION AND TESTS OF A SATELLITE ATTITUDE AND ORBIT CONTROL SYSTEM. GENERAL CONSIDERATIONS CONCERNING AN EXAMPLE CASE (INPE) AND DESIGN OF A SERVO RATE TABLE Fleury, Agenor deT. et al. National Aeronautics and Space Administration
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