Multiagent Attitude Control System for Satellites Based in Momentum Wheels and Event-Driven Synchronization

Author:

Garcia Juan L.,Moreno Jose Sanchez

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Reference17 articles.

1. Kristiansen, R., et al.: A comparative study of actuator configurations for satellite attitude control. Model. Identif. Control 26(4), 201–219 (2005)

2. Astolfi, A, Rapaport, A.: Robust stabilization of the angular velocity of a rigid body. Syst. Control Lett. 34, 256–264 (1998)

3. Guyot, P., et al.: Flywheel power and attitude control systems (FACS). In: Proceedings of the 4th ESA International Conference Spacecraft Guidance, Navigation and Control Systems, pp. 18–21. ESTEC, Noordwijk (1999)

4. Jiang, T., Khorasani, K.: A fault detection, isolation and reconstruction strategy for a satellite’s attitude control subsystem with redundant reaction wheels. In: IEEE International Conference on Systems, Man and Cybernetics, pp. 3146–3152, (ISIC, 2007), 7–10 Oct 2007

5. Karami, M.A., Sassani, F.: Spacecraft momentum dumping using less than three external control torques. In: IEEE International Conference on Systems, Man and Cybernetics, pp. 4031–4039, (ISIC, 2007), 7–10 Oct 2007

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