Spacecraft architecture for disturbance-free payload

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2002, Pages

  Pedreiro, Nelson ^a  

^a LOCKHEED MARTIN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

SPACECRAFT;

ANALYSIS AND SIMULATION; ISOLATION PERFORMANCE; NON- CONTACT SENSORS; SENSOR CHARACTERISTICS; SPACECRAFT ARCHITECTURE; SPACECRAFT DISTURBANCES; STABILITY REQUIREMENTS; VIBRATION ISOLATIONS;

SPACE FLIGHT;

EID: 85088346562     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-5029     Document Type: Conference Paper

References (9)

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2. Lee, A.Y. et al, "Preliminary Spacecraft Pointing Requirements Error Budgets for the Space Interferometry Mission", IEEE Aerospace Applications Conference Proceedings, v.4, pp. 35-47, 1999.
3. Bell, K.D. et al, "Air Force Research Laboratory's Technology Programs Addressing Deployable Space Optical Systems", SPIE-3356, pp. 535-551, 1998.
4. Lubomski, J.F. et al, "Final Report-Vibration Isolation Technology (VIT) ADT Project", NASA TM 106496, March 1994.
5. Laskin, R. A. and Sirlin, S. W., "Future Payload Isolation and Pointing System Technology", Journal of Guidance, Control and Dynamics, Vol. 9, No. 4, July-August 1986, pp. 469-477.
6. nd Congress of the International Astronautical Federation, Paper No. IAF-91-289, October 5-11, 1991, Montreal, Canada.
7. th International Cryogenic Engineering Conference, ICEC 12, pp. 455-459, 1988.
8. Mosier, G. et al, "Fine Pointing Control for a Next Generation Space Telescope", SPIE-3356, pp. 1070-1077, 1998.
9. Pedreiro, N., "Next Generation Space Telescope Pointing Stability", AIAA Paper 2000-4543, 2000.