论文信息 - Formation dynamics under a class of control laws

Formation dynamics under a class of control laws

A system of two earth satellites is analyzed as a controlled mechanical system. The orbit of an earth satellite can be represented by a point in the vector space of ordered pairs of angular momentum and Laplace vectors. Control laws are obtained by introducing a Lyapunov function on this space. Formations of two satellites are achieved asymptotically by the controlled dynamics.

Fumin Zhang | P.S. Krishnaprasad

[1] H. Schaub,et al. J2 Invariant Relative Orbits for Spacecraft Formations , 2001 .

[2] Perinkulam S. Krishnaprasad. Relative equilibria and stability of rings of satellites , 2000, Proceedings of the 39th IEEE Conference on Decision and Control (Cat. No.00CH37187).

[3] John L. Junkins,et al. Spacecraft Formation Flying Control using Mean Orbit Elements , 2000 .

[4] D. Chichka. Satellite Clusters with Constant Apparent Distribution , 2001 .

[5] Jerrold E. Marsden,et al. LYAPUNOV-BASED TRANSFER BETWEEN ELLIPTIC KEPLERIAN ORBITS , 2001 .