Robust Attitude Control Systems Design for Solar Sails (Part 2): MicroPPT-based Backup ACS
Author:
Affiliation:
1. Arizona State University
2. AEC-Able Engineering
3. Princeton Satellite Systems
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-5011
Reference11 articles.
1. Robust Attitude Control Systems Design for Solar Sails (Part 1): Propellantless Primary ACS
2. Development of a PPT for the EO-1 spacecraft
3. A micro pulsed plasma thruster (PPT) for the "Dawgstar" spacecraft
4. 5Rayburn, C., Campbell, M., and Mattick, A. "Pulsed Plasma Thruster System for Microsatellites," to appear in Journal of Spacecraft and Rockets, 2004.
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