Adaptive Synchronization Control of Multiple Spacecraft Formation Flying

Author:

Liu Hong-Tao1,Shan Jinjun2,Sun Dong3

Affiliation:

1. The Institute for Aerospace Studies, University of Toronto, 4925 Dufferin St., Toronto, Canada M3H 5T6

2. Department of Earth and Space Science and Engineering, York University, 4700 Keele St., Toronto, Canada M3J 1P3

3. Department of Manufacturing Engineering and Engineering Management, City University of Hong Kong, 83 Tat Chee Ave., Hong Kong

Abstract

An adaptive nonlinear synchronization control approach is developed for multiple spacecraft formation flying with elliptical reference orbits. It can guarantee that both the tracking errors and the synchronization errors of the relative positions converge to zero globally, even in the presence of uncertain parameters. The generalized synchronization concept allows us to design various synchronization errors so that different synchronization performance can be obtained. Simulation results of a leader-follower spacecraft pair and the maneuvering of multiple spacecraft in formation flying are presented to verify the effectiveness of the proposed control technique.

Publisher

ASME International

Subject

Computer Science Applications,Mechanical Engineering,Instrumentation,Information Systems,Control and Systems Engineering

Reference11 articles.

1. Formation Keeping for a Pair of Satellites in a Circular Orbit;Vassar;J. Guid. Control Dyn.

2. Decentralized Control of Satellite Formations;Carpenter;Int. J. Robust Nonlinear Control

3. An Intelligent Control Concept for Formation Flying Satellites;Vadali;Int. J. Robust Nonlinear Control

4. Adaptive Nonlinear Control of Multiple Spacecraft Formation Flying;de Queiroz;J. Guid. Control Dyn.

5. Adaptive Learning Control-Based Periodic Trajectory Tracking for Spacecraft Formations;Wong

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