Dynamics of a 3D rotating tethered formation flying facing the earth

IEEE Aerospace Conference Proceedings

Volumn , Issue , 2007, Pages

  Sabatini, Marco ^a   Palmerini, Giovanni B ^a  

^a SAPIENZA UNIVERSITY OF ROME   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; GRAVITATION; HARDWARE; MOTION CONTROL; ORBITS; SPACECRAFT;

CENTRIFUGAL FORCES; FISHNETS; FORMATION FLYING; GRAVITY GRADIENT;

FLIGHT DYNAMICS;

EID: 34548799676     PISSN: 1095323X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/AERO.2007.352671     Document Type: Conference Paper

References (18)

1. th International Astronautical Congress, Vancouver, 2004.
2. N. Takeichi, H. Ueno, M. Oda, "Feasibility study of a solar power satellite system configured by formation flying", Acta Astronáutica, vol.57 (2005), pp.698-706
3. C.D. Pengelley, "Preliminary survey of dynamic stability of a cable-connected spinning space station", Journal of Spacecraft and Rockets, 3:1456-1462, 1966.
4. J.V. Breakwell, "Stability of an orbiting ring. Journal of Guidance and Control", 4:197-200, March-April 1981.
5. V.V. Beletsky and E.M. Levin, "Stability of a ring of connected satellites", Acta Astronáutica, 12:765-769, 1985
6. E.C. Lorenzini, "A three-mass tethered system for micro-g/variable-g applications", Journal of Guidance, Control and Dynamics, 10:242-249, May-June 1987.
7. V. V. Beletsky, E. M. Levin, "Dynamics of space tether systems", Advances in the Astronautical Sciences, Volume 83, AAS publication, 1993
8. th October 2006, Valencia, Spain
9. A.B. DeCou, "Tether Static Shape for Rotating Multimass, Multitether, Spacecraft for Triangle Michelson Interferometer," Journal of Guidance, Control and Dynamics, Vol. 2, No. 2, March 1989, pp. 273-275.
10. S. Tragesser, "Formation Flying with Tethered Spacecraft," AIAA/AAS Astrodynamics Specialist Conference, Denver, CO, Aug. 2000, AIAA Paper 00-4133.
11. T. Williams and K. Moore, "Dynamics of tethered satellite formations", in AAS/AIAA Spaceflight Mechanics Meeting, San Antonio, Texas, 2002.Paper AAS 02-198.
12. S. Tragesser and A. Tuncay, "Orbital Design of EarthOriented Tethered Satellite Formations," AIAA/AAS Astrodynamics Specialist Conference and Exhibit, Monterey, CA, Aug. 2002, AIAA Paper 2002-4641.
13. P.C. Hughes, "Spacecraft Attitude Dynamics", John Wiley, New York, 1986.
14. th International Astronautical Congress, Fukuoka, Japan, 2005.
15. A.K. Misra, Z. Amier, and V. J. Modi, "Attitude dynamics of three-body tethered systems", Acta Astronautica, 17:1059-1068, 1988.
16. A. K. Misra and V. J. Modi, "Three-dimensional dynamics and control of tether-connected Nbody systems", Acta Astronautica, 26:77-84, 1992.
17. M. Keshmiri, A.K. Misra, and V. J. Modi, "General formulation for N-body tethered satellite system dynamics", Journal of Guidance, Control and Dynamics, 19:75-83, January 1996.
18. th October 2006, Valencia, Spain