Application of Hamiltonian structure-preserving control to formation flying on a J 2-perturbed mean circular orbit

Author:

Xu Ming,Zhu Jiamin,Tan Tian,Xu Shijie

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Astronomy and Astrophysics,Applied Mathematics,Computational Mathematics,Mathematical Physics,Modeling and Simulation

Reference43 articles.

1. Alfriend, K.T., Yan, H.: An orbital elements approach to the nonlinear formation flying problem. In: 1st International Formation Flying Symposium, Toulouse (2002)

2. Alfriend, K.T., Vadali, S., Gurfil, P., How, J., Breger, L.: Spacecraft Formation Flying: Dynamics, Control and Navigation. Elsevier Astrodynamics Series (2010)

3. Badawya A., McInnes C.: Small spacecraft formation using potential functions. Acta Astronaut. 65(11–12), 1783–1788 (2009)

4. Born G.H., Goldstein D.B., Thompson B.: An analytical theory for orbit determination. J. Astronaut. Sci. 49(2), 345–361 (2001)

5. Breger, L., How, P.: Partial J 2-invariance for Spacecraft Formations. In: AIAA/AAS Astrodynamics Conference, Keystone, AIAA 2006-6585 (2006)

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