Further results on the controllability of a two-wheeled satellite

Journal of Guidance, Control, and Dynamics

Volumn 30, Issue 2, 2007, Pages 611-619

  Boyer, Frédéric ^a,c   Alamir, Mazen ^b,d  

^a ECOLE DES MINES DE NANTES   (France)

^b GIPSA LAB   (France)

^c INSTITUT DE RECHERCHE EN COMMUNICATIONS ET CYBERNÉTIQUE DE NANTES   (France)

^d Domaine Universitaire   (France)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; CONTROLLABILITY; MOTION PLANNING; SPACECRAFT; STEERING;

KINETIC MOMENTUM; NONACTUATED SPACECRAFT AXIS; OPEN LOOP ATTITUDE CONTROL; REACTION WHEELS;

SATELLITES;

EID: 33947646404     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.21505     Document Type: Article

References (16)

1. Montgomery, R., "Gauge Theory and the Falling Cat," in Dynamics and Control of Mechanical Systems: The Falling Cat and Related Problems, edited by Michael J. Enos, American Mathematical Society, Providence, R.I., 1992.
2. Bonnard, B., "Controllabilité des Systèmes Mécaniques sur les Groupes de Lie," SIAM Journal on Control and Optimization, Vol. 22, No. 5, 1984, pp. 711-722.
3. Crouch, P. E., "Spacecraft Attitude Control and Stabilization: Applications of Geometric Control Theory to Rigid Body Models," IEEE Transactions on Automatic Control, Vol. 29, No. 4, 1984, pp. 321-331.
4. Morin, P., Samson, C., Pomet, J. B., and Jiang, Z. P., "Time Varying Feedback Stabilization of a Rigid Spacecraft with Two Controls," Systems and Control Letters, Vol. 25, No. 5, 1995, pp. 375-385.
5. Coron, J. M., and Kerai, E. Y., "Explicit Feedbacks Stabilizing the Attitude of a Rigid Spacecraft with Two Control Torques," Automatica, Vol. 32, No. 5, 1996, pp. 669-677.
6. Alamir, M., and Boyer, F., "Fast Generation of Attractive Trajectories for an underactuated Satellite, Application to Feedback Control Design" Optimization and Engineering, Vol. 4, 2003, pp. 215-230.
7. Tsiotras, P., and Doumtchenko, V., "Control of Spacecraft Subject to Actuator Failures: State-of-the-Art and Open Problems," Journal of the Astronautical Sciences, Vol. 48, Nos. 2 and 3, 2000, pp. 337-358.
8. Krishnan, H., Me Clamroch, N. H., and Reyhanoglu, M., "Attitude Stabilization of a Rigid Spacecraft Using Two Momentum Wheel Actuators," Journal of Guidance, Control, and Dynamics, Vol. 18, No. 2, 1995, pp. 256-263.
9. Horri, N. M., and Hodgart, S., "Attitude Stabilization of an Underactuated Satellite Using Two Wheels," Proceedings of the IEEEAC Conference, Vol. 6, 2002, pp. 2629-2635.
10. Kim, S., and Kim, Y., "Spin Axis Stabilization of a Rigid Spacecraft Using Two Reaction Wheels," Journal of Guidance, Control, and Dynamics, Vol. 24, No. 5, 2001, pp. 1046-1049.
11. Fliess, M., Lévine, J., Martin, Ph., and Rouchon, P., "Flatness and Defect of Nonlinear Systems: Introductory Theory and Examples," International Journal of Control, Vol. 44, No. 5, 1999, pp. 922-937.
12. Alamir, A., and Marchand, N., "Numerical Stabilisation of Non-Linear Systems: Exact Theory and Approximate Numerical Implementation," European Journal of Control, Vol. 5, 1999, pp. 87-97.
13. Tsiotras, P., and Longuski, J. M., "Spin-Axis Stabilization of Symmetric Spacecraft with Two Control Torques," Systems and Control Letters, Vol. 23, 1994, pp. 395-402.
14. Tsiotras, P., and Longuski, J. M., "A New Parameterization of the Attitude Kinematics," Journal of the Astronautical Sciences, Vol. 43, No. 3, 1995, pp. 243-262.
15. Tsiotras, P., Corless, M., and Longuski, J. M., "A Novel Approach to the Attitude Control of an Axisymmetric Spacecraft," Automatica, Vol. 31, No. 8, 1995, pp. 1099-1112.
16. Petersen, P., "Symmetric Spaces and Holonomy," Riemannian Geometry, Graduate Texts in Mathematics, Springer, New York, 1998, pp. 205-242.