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Cites:

Information Journal Paper

Title

ROBUST ADAPTIVE CONTROL OF THE SPACECRAFT FORMATION FLYING IN HIGH ECCENTRICITY ELLIPTICAL ORBIT

Pages

  83-96

Abstract

 In this paper, the issue of robust control of the spacecraft formation flying will be discussed. For this purpose two high order sliding mode controller (HOSMC) are designed for nonlinear spacecraft formation flying in leader-follower structure. The SMC- super twisting algorithm is applied due to chattering reduction and so SMC- nonsingular terminal is applied due to finite time convergence. In the design of both controllers, the actuator saturations is considered.To reduce the control effort, the adaptive gains are applied. The gains of robust controllers are adapted due to the error measurement or conditions. Both ADAPTIVE SUPER TWISTING and terminal sliding mode are proposed on the PROBA-3 Space mission. The controllers' performances are examined in formation flying maneuvers with large eccentricity considering uncertainty and J2 disturbance.

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  • Cite

    APA: Copy

    MALEKZADEH, M., RABIEI, A., & ABNILI, M.. (2017). ROBUST ADAPTIVE CONTROL OF THE SPACECRAFT FORMATION FLYING IN HIGH ECCENTRICITY ELLIPTICAL ORBIT. JOURNAL OF SOLID AND FLUID MECHANICS, 7(3 ), 83-96. SID. https://sid.ir/paper/212808/en

    Vancouver: Copy

    MALEKZADEH M., RABIEI A., ABNILI M.. ROBUST ADAPTIVE CONTROL OF THE SPACECRAFT FORMATION FLYING IN HIGH ECCENTRICITY ELLIPTICAL ORBIT. JOURNAL OF SOLID AND FLUID MECHANICS[Internet]. 2017;7(3 ):83-96. Available from: https://sid.ir/paper/212808/en

    IEEE: Copy

    M. MALEKZADEH, A. RABIEI, and M. ABNILI, “ROBUST ADAPTIVE CONTROL OF THE SPACECRAFT FORMATION FLYING IN HIGH ECCENTRICITY ELLIPTICAL ORBIT,” JOURNAL OF SOLID AND FLUID MECHANICS, vol. 7, no. 3 , pp. 83–96, 2017, [Online]. Available: https://sid.ir/paper/212808/en

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