International space station assembly and operation control challenges

Advances in the Astronautical Sciences

Volumn 104, Issue , 2000, Pages 259-271

  Bedrossian, Nazareth ^a  

^a Charles Stark Draper Laboratory Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0039766983     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

References (16)

1. NASA/Boeing, "International Space Station GN&C Design Guidelines and Assumptions", Revision B, 1997.
2. Hall, R., Kirchwey, K., Martin, M., Rosch, G., Zimpfer, D., "Flight Control Overview of STS-88, The First Space Station Assembly Flight", Procc 1999 AAS/AIAA Astrodynamics Conference, AAS Paper No. 99-371, Aug. 1999
3. RSC-Energia, "ISS Item 17Km N128 Terminal Computer Software Guidance, Navigation and Control System Information Memorandum", Software Version 4.0 Document, 1999.
4. Zimpfer, D., Kirchwey, K., Hanson, D., Jackson, M., and Smith, N., "Shuttle Stability And Control Of the STS-71 Shuttle/MIR Mated Configuration", Proc. 1996 AAS/AIAA Spaceflight Mechanics Conference, AAS Paper No. 96-131, Feb. 1996.
5. Bedrossian, N., "SSRMS Loads During CMG Desaturation", Draper Memo SSDI-94-011, Jul. 1994
6. Meckl, P. H., and Seering, W. P., "Minimizing Residual Vibration for Point-to-Point Motion", Journal of Vibration, Acoustics, Stress and Reliability in Design, Vol. 107, Oct. 1985, pp. 378-382.
7. Seering, W. P., and Singer, N. C., "Using Acausal Shaping Techniques to Reduce Robot Vibration", Proc. 1988 IEEE International Conference on Robotics and Automation, Apr. 1988, pp. 1434-1437.
8. Wie, B., Space Vehicle Dynamics and Control, AIAA Education Series, 1998.
9. Kubiak, E. T., and Sargent, D., "CR 89921C: Alternate Primary Jet Mode", Presentation to the Shuttle Avionics Software Control Board, Johnson Space Center, Houston TX, Jun. 1989.
10. Bedrossian, N, Lepanto, J., Adams, N., Sunkel, J., and Hua, T., "Jet Firing Strategy To Minimize Structural Loads", Proc. 1995 American Control Conference, pp. 3622-3626.
11. Vadali, S. R., and Junkins, J. L., "Optimal Open-Loop and Stable Feedback Control of Rigid Spacecraft Attitude Maneuvers," Journal of the Astonautical Sciences, Vol. 32, No. 2, 1984, pp. 105-122.
12. Carrington, C. K., and Junkins, J. L., "Spacecraft Attitude Control Using Generalized Angular Momenta", Proc. AIAA/AAS Astrodynamics Conference, AAS Paper No. 85-361, Aug. 1985.
13. Bedrossian, N., and McCants, E., "Space Station Attitude Control During Payload Operations", Proc. 1999 AAS/AIAA Astrodynamics Conference, AAS Paper No. 99-372, Aug. 1999.
14. Hughes, P. C., Spacecraft Attitude Dynamics, J. Wiley & Sons, 1986.
15. Elgersma, M. R., and Chang, D. S., "Determination of Torque Equilibrium Attitude For Orbiting Space Station", AIAA, 1992.
16. "International Space Station Robotic Assembly Analysis For Design Analysis Cycle#5, Flights UF1 Through 12A" DAC 5 Document, NASA JSC-38409.