Robust attitude control systems design for solar sails, part 2: MicroPPT-based secondary ACS

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference

Volumn 2, Issue , 2004, Pages 1325-1340

  Wie, Bong ^a,d   Murphy, David ^b,d   Paluszek, Michael ^c,d   Thomas, Stephanie ^c,d  

^a ARIZONA STATE UNIVERSITY   (United States)

^b NORTHROP GRUMMAN CORPORATION   (United States)

^c Princeton Satellite Systems Inc   (United States)

^d Dept of Mechanical and Aerospace Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; MANEUVERABILITY; PROPELLANTS; ROBUSTNESS (CONTROL SYSTEMS); SPACE RESEARCH; SYSTEMS ANALYSIS;

ATTITUDE CONTROL SYSTEMS (ACS); PULSED PLASMA THRUSTERS (PPT); SAIL MISSIONS; SOLAR SAILS;

SPACECRAFT;

EID: 19644382746     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. Wie, B., Murphy, D., Paluszek, M., and Thomas, S., "Robust Attitude Control Systems Design for Solar Sails, Part 1: Propellantless Primary ACS," AIAA-2004-5010, AIAA Guidance. Navigation, and Control Conference, Providence, RI, August 16-19, 2004.
2. Micci, M. and Ketsdever, A. (ed.), Micropropulsion for Small Spacecraft, Progress in Astronautics and Aeronautics, Volume 187, AIAA, Washington, DC, 2000, Chapter 3.
3. Benson, S., Arlington, L., Hoskins, A., and Meckel, N., "Development of a PPT for the EO-1 Spacecraft," AIAA-99-2276, 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Los Angeles, CA, June 20-24, 1999.
4. Cassady, R., Hoskins, A., Campbell, M., and Rayburn, C., "A Micro Pulsed Plasma Thruster (PPT) for the Dawgstar Spacecraft," Proceedings of the 2000 IEEE Aerospace Conference, Big Sky, Montana, 2000.
5. Rayburn, C., Campbell, M., and Mattick, A., "Pulsed Plasma Thruster System for Microsatellites," to appear in Journal of Spacecraft and Rockets, 2004.
6. Spanjers, G., Bromaghim, D., Lake, J., Dulligan, M., White, D., Schilling J., Bushman, S., Antonsen, E., Burton, R., Keidar, M., and Boyd, I., "AFRL MicroPPT Development for Small Spacecraft Propulsion," AIAA-2002-3974, 28th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, IN, July 2002.
7. Spanjers, G. et al., "High Stiffness Boom to Increase the Moment-Arm for a Propulsive Attitude Control System on FalconSat 3," presented at the AIAA Space Technologies Conference, Albuquerque. New Mexico, 2003. Also
8. FalconSat3 web site: www.skyrocket.de/space/doc-sdat/falconsat-3.htm.
9. Pryor, K., Wie, B., and Mikollidns, P., "Development of a Lightweight Pulsed Plasma Thruster Modulo for Solar Sail Attitude Control," Paper SSC04-XI-4, 18th Annual AIAA/USU Conference on Small Satellite, Logan, Utah, August 9-12, 2004.
10. Wie, B., "A Low-Cost, Low-Mass, Low-Powor, and Low-Volume Attitude Determination and Control System for Solar Sail Spacecraft," U.S. Patent Application, File No. 60/433,053, August 13, 2003 (Provisional Invention Disclosure: ASU Case No. MS 3-029, Ortober 2002).
11. Lappas, V., Wie, B., McInnes, C., Tarabini, L., Gomes, L., and Wallace, K., "Design of a Solar Kite Mission to Study the Earth's Magnetotail," Paper SSC04-VI-3, 18th Annual AIAA/USU Conference on Small Satellites, Logan, Utah, August 9-12, 2004.
12. Anthony, T., Wie, B. and Carroll, S., "Pulse-Modulated Controller Synthesis for a Flexible Spacecraft," Journal of Guidance. Control, and Dynamic, Vol. 13, No. 6, 1990, pp. 1014-1022.