Adaptive Nonlinear Controller for Quadrotor Altitude Control with Online Control Coefficients Function

Publish Year: 1402
نوع سند: مقاله ژورنالی
زبان: English
View: 46

This Paper With 7 Page And PDF Format Ready To Download

  • Certificate
  • من نویسنده این مقاله هستم

استخراج به نرم افزارهای پژوهشی:

لینک ثابت به این Paper:

شناسه ملی سند علمی:

JR_MJEE-17-4_004

تاریخ نمایه سازی: 16 دی 1402

Abstract:

In this paper, an adaptive controller is presented to control a quadrotor, whose parameters are extracted from the genetic algorithm optimization method. The advantage of this method is that based on the system states, the control coefficients are calculated online. For this purpose, a function between system states-space and control coefficients is obtained. From the database collected from the genetic algorithm optimization method, the parameters of the control coefficient function are obtained using the least squares method. The stability of the proposed controller is proved by the Lyapunov method. Finally, the performance of the proposed controller is compared with the PID controller, which is widely used in the literature. The results show that the proposed approach is promising.

Authors

Alireza Ahangarani Farahani۱

Department of Aerospace Engineering, Malek Ashtar University of Technology, Tehran, Iran

Sayyed Majid Hosseini

Department of Aerospace Engineering, Malek Ashtar University of Technology, Tehran, Iran

meysam delalat

Department of Aerospace Engineering, Malek Ashtar University of Technology, Tehran, Iran

مراجع و منابع این Paper:

لیست زیر مراجع و منابع استفاده شده در این Paper را نمایش می دهد. این مراجع به صورت کاملا ماشینی و بر اساس هوش مصنوعی استخراج شده اند و لذا ممکن است دارای اشکالاتی باشند که به مرور زمان دقت استخراج این محتوا افزایش می یابد. مراجعی که مقالات مربوط به آنها در سیویلیکا نمایه شده و پیدا شده اند، به خود Paper لینک شده اند :
  • Zhao, D. Wang, Q. –e. Zhao, J. Hu and Q. ...
  • M. M. Dehghan., A. Parsa, A. Ahangarani Farahani and E. ...
  • Islam, M. Okasha and M.M. Idres, “Trajectory tracking in quadrotor ...
  • A. Najm, I. K. Ibraheem, “Nonlinear PID controller design for ...
  • Zhou, B. Zhang, “Quadrotor UAV flight control using backstepping adaptive ...
  • Qiao, Z. Liu, and Y. Zhang, “Gain scheduling PID control ...
  • Navabi, and H. Mirzaei, “Robust optimal adaptive trajectory tracking control ...
  • Shi, Y. Cheng, C. Yin, S. Dadras and X. Huang, ...
  • Edjghou, N. Slimane and K. Chafaa, “Fuzzy sliding mode control ...
  • Samantaray and S. Chakrabarty, “A fuzzy sliding mode control design ...
  • Sanz, P. Garcia, Q. Zhong and P. Albertos, “Robust control ...
  • Zhao, B. Xian, Y. Zhang and X. Zhang, “Nonlinear robust ...
  • J. Wu, H. Tang and X. –Z. Jin, “Robust adaptive ...
  • X. Mung and S. K. Hong, “Robust backstepping trajectory tracking ...
  • Ahangarani Farahani, “Controller designed based on feedback linearization technique for ...
  • K. Tan, J. Wang, Y. C. Paw and T. Y. ...
  • –C, Liu and T. –W. Ou, “Non-linear adaptive tracking control ...
  • Huang, D. Huang, Z. Wang, and A. Shah, “Robust tracking ...
  • Khalil, “Nonlinear systems”, Prentice Hall, Third edition, ۲۰۲۰ ...
  • Ahangarani Farahani and J. Karimi, “Adaptive controller design to Euler ...
  • نمایش کامل مراجع