Governed by: Ministry of Industry and Information Technology of the People's Republic of China
Sponsored by: Northwestern Polytechnical University  Chinese Society Aeronautics and Astronautics
Address: Aviation Building,Youyi Campus, Northwestern Polytechnical University
Attitude control of small quadrotor Based on ADRC Theory
DOI:
Author:
Affiliation:

Northwestern Polytechnical University,Northwestern Polytechnical University

Clc Number:

V235

Fund Project:

  • Article
  • |
  • Figures
  • |
  • Metrics
  • |
  • Reference
  • |
  • Related
  • |
  • Cited by
  • |
  • Materials
  • |
  • Comments
    Abstract:

    To solve the attitude control problem of small quadrotor according to its complex coupling, non-linear and serious internal/external disturbance feature, a control scheme based on active disturbance rejection control technique is proposed. The dynamic model is established with Newton-Euler formalism, and the uncertainty, coupling and parameter perturbation are considered as total disturbance. Extended State Observer is used to estimate and compensate the total disturbance, the Non-linear State Error Feedback is used to restrain the compensate error, a model for simulation is established. The result of the simulation shows that the Extended State Observer of the Active Disturbance Rejection Control technique can estimate/compensate disturbance well under circumstance of parameter perturbation and disturbance. Attitude controller based on Active Disturbance Rejection Control theory shows good dynamic quality, steady-state accuracy and strong robustness.

    Reference
    Related
    Cited by
Get Citation

Zhang Guangyu, Yuan Changsheng. Attitude control of small quadrotor Based on ADRC Theory[J]. Advances in Aeronautical Science and Engineering,2014,5(3):

Copy
Share
Article Metrics
  • Abstract:
  • PDF:
  • HTML:
  • Cited by:
History
  • Received:December 10,2013
  • Revised:January 21,2014
  • Adopted:February 24,2014
  • Online: June 23,2016
  • Published: