PL EN


Preferencje help
Widoczny [Schowaj] Abstrakt
Liczba wyników
Tytuł artykułu

Ultimate state boundedness of underactuated spacecraft subject to an unmatched disturbance

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
Ultimate state boundedness for underactuated spacecraft subject to large non-matched disturbances is attained. First, non-smooth time-invariant state feedback control laws that make the origin asymptotically stable are obtained. Then, the controller is extended to make the closed-loop system globally uniformly ultimately bounded under the following conditions: 1) the disturbances acting on the directly actuated states are known and 2) the disturbance acting on the unactuated state is bounded and its profile need not be known. Finally, numerical simulations are presented to verify the analytical results. A large step disturbance is considered, and it is shown that the proposed controller makes the closed-loop system globally uniformly ultimately bounded. The proposed method is rather general and can be extended to other systems.
Rocznik
Strony
1055--1066
Opis fizyczny
Bibliogr. 15 poz., rys., tab.
Twórcy
autor
  • Aerospace Research Institute (Ministry of Science, Research and Technology), Tehran, Iran
autor
  • Aerospace Research Institute (Ministry of Science, Research and Technology), Tehran, Iran
  • Department of Aerospace Engineering, Sharif University of Technology, Tehran, Iran
Bibliografia
  • 1. Aneke N.P.I., 2003, Control of Underactuated Mechanical Systems, Eindhoven: Technische Universitat Eindhoven, DOI: 10.6100/IR559509
  • 2. Astolfi A., Rapaport A., 1998, Robust stabilization of the angular velocity of a rigid body, Systems and Control Letters, 34, 5, 257-264, DOI: 10.1016/S0167-6911(98)00031-0
  • 3. Choukchou-Braham A., Cherki B., Djemai M., Busawon K., 2013, Analysis and Control of Underactuated Mechanical Systems, Springer, DOI: 10.1007/978-3-319-02636-7
  • 4. Fantoni I., Lozano R., 2002, Nonlinear Control for Underactuated Mechanical Systems, Springer-Verlag London, Communication and Control Engineering, ISBN: 978-1-4471-1086-6, DOI: 10.1007/978-1-4471-0177-2
  • 5. Floquet T., Perruquetti W., Barbot J.P., 2000, Angular velocity stabilization of a rigid body via VSS control, Journal of Dynamic Systems, Measurement, and Control, 122, 4, 669-673, DOI:10.1115/1.1316787
  • 6. Karami M.A., Sassani F., 2007, Nonlinear attitude control of an underactuated spacecraft subject to disturbance torques, Proceedings of the American Control Conference, 3150-3155, DOI: 10.1109/ACC.2007.4283042
  • 7. Khalil H., 2000, Nonlinear Systems, Prentice Hall, Third Edition, ISBN: 0-13-067389-7
  • 8. Liu Y., Yu H., 2013, A survey of underactuated mechanical systems, IET Control Theory and Applications, 7, 7, 921-935, DOI: 10.1049/iet-cta.2012.0505
  • 9. Olfati-Saber R., 2001, Nonlinear control of underactuated mechanical systems with application to robotics and aerospace vehicles, Ph.D. Thesis, MIT University
  • 10. Reyhanoglu M., 1996, Discontinuous feedback stabilization of the angular velocity of a rigid body with two control torques, Proceedings of the 36th IEEE Conference on Decision and Control, 3, 2692-2694, DOI: 10.1109/CDC.1996.573511
  • 11. Reyhanoglu M., Cho S., McClamroch H.N., 2000, Discontinuous feedback control of a special class of underactuated mechanical systems, International Journal of Robust and Nonlinear Control, 10, 4, 265-281, DOI: 10.1002/(SICI)1099-1239(20000415)10:43.0.CO;2-N
  • 12. Sidi M.J., 2000, Spacecraft Dynamics and Control: A Practical Engineering Approach, Cambridge Aerospace Series 7, ISBN: 0-521-55072-6
  • 13. Spong M.W., 1998, Underactuated mechanical systems, Control Problems in Robotics and Automation, Lecture Notes in Control and Information Sciences, 230, 135-150, DOI: 10.1007/BFb0015081
  • 14. Wang D., Jia Y., Jin L., Xu S., 2013, Control analysis of an underactuated spacecraft under disturbance, Acta Astronautica, 83, 44-53, DOI: 10.1016/j.actaastro.2012.10.029
  • 15. Zhang H.H., Wang F., Trivailo P.M., 2008, Spin-axis stabilization of underactuated rigid spacecraft under sinusoidal disturbance, International Journal of Control, 81, 12, 1901-1909, DOI: 10.1080/00207170801930217
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-07b784f0-6f74-46ab-bfa7-3a0c808cdbd3
JavaScript jest wyłączony w Twojej przeglądarce internetowej. Włącz go, a następnie odśwież stronę, aby móc w pełni z niej korzystać.