Dual Manipulator-Actuated Integrated Translational and Rotational Stabilization of Spacecraft in Proximity Operations

Author:

ZHANG Feng1,LI Yang1,YAN Ning1

Affiliation:

1. Research and Development Department, China Academy of Launch Vehicle Technology

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Reference22 articles.

1. 1) Terui, F.: Position and Attitude Control of a Spacecraft by Sliding Mode Control, Proceedings of American Control Conference, Jun. 1998, pp. 217–221.

2. 2) Kristiansen, R., Nicklasson, P., and Gravdahl, J.: Spacecraft Coordination Control in 6DOF: Integrator Backstepping vs Passivity-based Control, Automatica, 44 (2008), pp. 2896–2901.

3. 3) Shan, J.: Six-DOF Synchronised Adaptive Learning Control for Spacecraft Formation Flying, IET Control Theory Appl., 2 (2008), pp. 930–949.

4. 4) Xin, M. and Pan, H.: Integrated Nonlinear Optimal Control of Spacecraft in Proximity Operations, Int. J. Control, 83 (2010), pp. 347–363.

5. 5) Wang, J., Liang, H., Sun, Z., Zhang, S., and Liu, M.: Finite-time Control for Spacecraft Formation with Dual-number Based Description, J. Guid. Control Dynam., 35 (2012), pp. 950–962.

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