COMPENSATING STRUCTURE AND PARAMETER OPTIMIZATION FOR ATTITUDE CONTROL OF A FLEXIBLE SPACECRAFT | 東京工業大学附属図書館文献データベース

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COMPENSATING STRUCTURE AND PARAMETER OPTIMIZATION FOR ATTITUDE CONTROL OF A FLEXIBLE SPACECRAFT

著者名:: Ceballos, D.C. ( Instituto de Pesquisas Espaciais, Sao Jose )
掲載資料名:: NASA Technical Reports
発行年:: 1985
号:: INPE-3564-PRE 770
通号:: G6/18 03532
ペーパー番号:: N86-17371
開始ページ:: 1
終了ページ:: 24
総ページ数:: 24
出版情報:: National Aeronautics and Space Administration
言語:: 英語
資料種別:: テクニカルペーパー

詳細

TDL書誌ID:

ZA00001422

類似資料:

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5 テクニカルペーパー Robust Nonlinear Attitude Control of Spacecraft with Flexible Structures Lin,Y.-Y., Lin,G.-L. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Control and Structural Optimization for Maneuvering Large Spacecraft Chun, H.M., Turner, J.D., Yu, C.C. National Aeronautics and Space Adminstration
6 テクニカルペーパー Vibration Control of Flexible Spacecraft Under Attitude Maneuver Using Adaptive Controller C. Oh, H. Bang, J. Park American Institute of Aeronautics and Astronautics	12 テクニカルペーパー MACE II: a space shuttle experiment for investigating adaptive control of flexible spacecraft Denoyer, Keith K., Hyland, David C., Davis, Lawrence D., Miller, David W. American Institute of Aeronautics and Astronautics

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