Underactuated Steering Control Law for Spacecraft Attitude Maneuver using Two Skewed Control Moment Gyroscopes under Path Constraint
Author:
Affiliation:
1. Department of Aerospace Engineering, Tokyo Metropolitan University
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/tjsass/67/5/67_T-23-29/_pdf
Reference36 articles.
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2. 2) Tsiotras, P. and Longuski, J. M.: Spin-axis Stabilization of Symmetric Spacecraft with Two Control Torques, Syst. Control Lett., 23 (1994), pp. 395–402.
3. 3) Zavoli, A., Matteis, G. D., Giulietti, F., and Avanzini, G.: Single-axis Pointing of an Underactuated Spacecraft Equipped with Two Reaction Wheels, J. Guid. Control Dynam., 40 (2017), pp. 1465–1471.
4. 4) Brockett, R. W.: Asymptotic Stability and Feedback Stabilization, Differential Geometric Control Theory, 27 (1983), pp. 181–191.
5. 5) Aeyels, D. and Szafransski, M.: Comments on the Stabilizability of the Angular Velocity of a Rigid Body, Syst. Control Lett., 10 (1988), pp. 35–39.
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