J2 dynamics and formation flight

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2001, Pages

  Koon, Wang Sang ^a   Marsden, Jerrold E ^a   Murray, Richard M ^a   Masdemont, Josep ^b  

^a CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

^b UNIVERSITAT POLITÈCNICA DE CATALUNYA   (Spain)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894493382     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Sedwick, R.J., E.M.C. Kong and D.W. Miller [1998] Exploring orbital dynamics and micropropulsion for aperture synthesis using distributed satellite systems: applications to techsat 21, AIAA-98-5289.
2. 2 invariant reference orbits for spacecraft formations, Flight Mechanics Symposium, Goddard Space Flight Center, May 18-20.
3. Brouwer, D. [1959] Solution of the problem of artificial satellite theory without drag, The Astronautical Journal 64, No. 1274, 478-397.
4. Koon, W.S, M.W. Lo, J.E. Marsden and S.D. Ross [2000] Heteroclinic connections between periodic orbits and resonance transitions in celestial mechanics, Chaos 10 No. 2, 427-469.
5. Broucke, R.A. [1994] Numerical integration of periodic orbits in the main problem of artificial satellite theory, Celestial Mechanics and Dynamical Astronomy 58, 99-123.
6. Deprit, A. and A. Rom [1970] The main problem of artificial satellite theory for small and moderate eccentricities, Celestial Mechanics 2 (1970), 166-206.
7. Milam, M.B., N. Petit and R.M. Murray [2001], Constrained trajectory generation for micro satellite formation flying. The proceedings of AIAA Guidance, Navigation and Control Conference, August, 2001, Montreal, Canada.
8. Petit, N., M.B. Milam and R.M. Murray [2001] Inversion based constrained trajectory optimization. The proceedings of the 5th IFAC Symposium on Nonlinear Control Systems, 2001.