Thruster actuation algorithms for scientific space...-Reference-Cited by-同舟云学术

Thruster actuation algorithms for scientific space...

Published:2005-10-17 Issue: Volume: Page:
ISSN:
Container-title:56th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law
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Author:

Bindel Daniel¹,Schlotterer Markus¹,Theil Stephan¹

Affiliation:

1. Center of Applied Space Technology and Microgravity, University of Bremen, Am Fallturm, D-28359 Bremen, Germany

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.IAC-05-C1.P.10

Reference7 articles.

1. Jeng-Heng Chen. Helium Thruster Propulsion System for Precise Attitude Control and Drag Compensation of the Gravity Probe-B Satellite. PhD thesis,Department of Aeronautics and Astronautics, Stanford University, December 1983.

2. A. Genovese, M. Tajmar, N. Buldrini, M. Scheerer, E. Semerad, and W. Steiger. Indium FEEP Multiemitter Development and Test Results. In 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, July 2004. AIAA-2004-3620.

3. HaiPing Jin. Translation and Attitude Control for the QUICK-STEP Satellite. PhD thesis,Department of Aeronautics and Astronautics of Stanford University, August 1996.

4. A. Schleicher. Thruster actuation algorithm design and analysis. Technical Report S2-ZARTN-2001, ZARM, July 2004.

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