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Information Journal Paper

Title

MULTI-AXIS ATTITUDE MANEUVER OF A FLEXIBLE SPACECRAFT USING ADAPTIVE HYBRID SLIDING MODE CONTROL

Pages

  59-68

Abstract

 A new control strategy for attitude maneuver of an elastic spacecraft is presented. ADAPTIVE SLIDING MODE control scheme with a synthesized HYBRID SLIDING SURFACE (HSS) is used to overcome the difficulties arising from measurement of flexible dynamics coordinates. The excitation of flexible modes that frequently happens in the conventional sliding mode is minimized by using the synthesized sliding surface. The model of the spacecraft considered as rigid central hub and two flexible appendages. Collocated actuators and sensors are placed on the rigid central hub. Stability proof of the overall closed-loop system is given via Lyapunov analysis. Asymptotical tracking control of the multi-axis attitude motion and suppression of the elastic deformations are accomplished. Numerical simulations show the effectiveness of the proposed control scheme.

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    APA: Copy

    KABGANIAN, M., SHAHRAVI, M., & ALASTI, A.. (2006). MULTI-AXIS ATTITUDE MANEUVER OF A FLEXIBLE SPACECRAFT USING ADAPTIVE HYBRID SLIDING MODE CONTROL. AMIRKABIR, 16(63-B), 59-68. SID. https://sid.ir/paper/541384/en

    Vancouver: Copy

    KABGANIAN M., SHAHRAVI M., ALASTI A.. MULTI-AXIS ATTITUDE MANEUVER OF A FLEXIBLE SPACECRAFT USING ADAPTIVE HYBRID SLIDING MODE CONTROL. AMIRKABIR[Internet]. 2006;16(63-B):59-68. Available from: https://sid.ir/paper/541384/en

    IEEE: Copy

    M. KABGANIAN, M. SHAHRAVI, and A. ALASTI, “MULTI-AXIS ATTITUDE MANEUVER OF A FLEXIBLE SPACECRAFT USING ADAPTIVE HYBRID SLIDING MODE CONTROL,” AMIRKABIR, vol. 16, no. 63-B, pp. 59–68, 2006, [Online]. Available: https://sid.ir/paper/541384/en

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