مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

video

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

sound

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Persian Version

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

View:

439
مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Download:

282
مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Cites:

Information Journal Paper

Title

ROBUST CONTROL OF NON-LINEAR FLEXIBLE SPACECRAFT

Pages

  217-228

Abstract

 In this paper, the problem of attitude control of a 1D non-linear flexible spacecraft is investigated. Three controllers are presented. The first is a non-linear DYNAMIC INVERSION, the second is a linear m-synthesis and the third is a composition of DYNAMIC INVERSION and a m-synthesis controller. It is assumed only one reaction wheel is used. ACTUATOR SATURATION is considered in the design of controllers. The performances of the proposed controllers are compared in terms of nominal performance, robustness to uncertainties, vibration suppression of panels, sensitivity to measurement noise, environment disturbance and non-linearity in large maneuvers. To evaluate the performance of the proposed controllers, an extensive number of simulations on a non-linear model of the spacecraft are performed. Simulation results show the ability of the proposed controller in tracking the attitude trajectory and damping panel vibration. It is also verified that the perturbations, environment disturbance and measurement errors have only slight effects on the tracking and damping responses.

Multimedia

  • No record.
  • Cites

  • No record.
  • References

  • No record.
  • Cite

    APA: Copy

    MALEKZADEH, M., NAGHASH, A., & TALEBI, H.A.. (2010). ROBUST CONTROL OF NON-LINEAR FLEXIBLE SPACECRAFT. SCIENTIA IRANICA, 17(3 (TRANSACTION B: MECHANICAL ENGINEERING)), 217-228. SID. https://sid.ir/paper/289952/en

    Vancouver: Copy

    MALEKZADEH M., NAGHASH A., TALEBI H.A.. ROBUST CONTROL OF NON-LINEAR FLEXIBLE SPACECRAFT. SCIENTIA IRANICA[Internet]. 2010;17(3 (TRANSACTION B: MECHANICAL ENGINEERING)):217-228. Available from: https://sid.ir/paper/289952/en

    IEEE: Copy

    M. MALEKZADEH, A. NAGHASH, and H.A. TALEBI, “ROBUST CONTROL OF NON-LINEAR FLEXIBLE SPACECRAFT,” SCIENTIA IRANICA, vol. 17, no. 3 (TRANSACTION B: MECHANICAL ENGINEERING), pp. 217–228, 2010, [Online]. Available: https://sid.ir/paper/289952/en

    Related Journal Papers

  • No record.
  • Related Seminar Papers

  • No record.
  • Related Plans

  • No record.
  • Recommended Workshops






    Move to top
    telegram sharing button
    whatsapp sharing button
    linkedin sharing button
    twitter sharing button
    email sharing button
    email sharing button
    email sharing button
    sharethis sharing button