Quasi-periodic J2 Invariant Relative Orbits for Formation Flying

Author:

Luo Qiang,Zheng Yaru,Xu Ming

Publisher

Springer Singapore

Reference9 articles.

1. Montenbruck O, Kirschner M, D’Amico S, Bettadpur S (2006) E/I-vector separation for safe switching of the GRACE formation. Aerosp Sci Technol 10(7):628–635

2. D’Amico S, Montenbruck O (2006) Proximity operations of formation flying spacecraft using an eccentricity/inclination vector separation. J Guid Control Dyn 29(3):554–563

3. Carter T, Humi M (2003) The Clohessy-Wiltshire equations can be modified to include quadratic drag. In: 13th AAS/AIAA space flight mechanics meeting, Ponce, Paper AAS 03-240

4. Izzo D, Sabatini M, Valente C (2003) A new linear model describing formation flying dynamics under J2 effects. In: Proceedings of 17th AIDAA national congress, Rome, vol 1, pp 493–500

5. Schweighart S, Sedwick R (2002) High-fidelity linearized J2 model for satellite formation flight. J Guid Control Dyn 25(6):1073–1080

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