Optimal Control for Spacecraft Large Angle Manuevers Using H infinity Linear Varying Parameter Control Techniques
- 著者名:
- 掲載資料名:
- AIAA meeting papers on disc
- シリーズ名:
- AIAA Paper : AIAA Guidance Navigation and Control Conference
- シリーズ巻号:
- 2008
- 発行年:
- 2008
- 通号:
- 2008-7311
- ペーパー番号:
- AIAA 2008-7311
- 出版情報:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- 言語:
- 英語
- 請求記号:
- A07400/200810 [CD-ROM 2008 Disc 10]
- 資料種別:
- テクニカルペーパー
類似資料:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
テクニカルペーパー
Linear Parameter Varying Control Synthesis for Actuator Failure, Based on Estimated Parameter
American Institute of Aeronautics and Astronautics |
8
テクニカルペーパー
Control of Large Micro-Spacecraft Formations Based on Quasi-Distributed-Parameter Models
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
10
テクニカルペーパー
Wide-range stabilization of an arm-driven inverted pendulum using linear parameter-varying techniques
American Institute of Aeronautics and Astronautics |
Society of Automotive Engineers |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |