• DocumentCode
    164153
  • Title

    Controller development and validation for a small quadrotor with compensation for model variation

  • Author

    Chen Wang ; Nahon, Meyer ; Trentini, Michael

  • Author_Institution
    Sch. of Aeronaut., Northwestern Polytech. Univ. in Xi´an, Xi´an, China
  • fYear
    2014
  • fDate
    27-30 May 2014
  • Firstpage
    902
  • Lastpage
    909
  • Abstract
    The research discussed here proposes a control system with compensation to maintain consistent performance for quadrotors under system variations, specifically due to battery drainage and mass changes. This compensation control system is comprised of three subsystems. The first subsystem is a baseline PID controller, which generates a desired rpm for each motor. The second subsystem compensates for battery drainage. Based on a complete relationship of PWM-rpm-Voltage obtained from experiments, this compensation subsystem calculates an appropriate PWM command needed to obtain the rpm received from the PID controller, taking into account the current battery voltage. The last subsystem consists of an online mass estimator to estimate the total mass of the quadrotor and payload, and correspondingly adapts the output of the PID controller in order to maintain performance. Simulation and experiments were conducted, both with and without the compensation strategies. The results clearly show the effectiveness of the proposed approaches.
  • Keywords
    aircraft control; compensation; control system synthesis; electric motors; helicopters; pulse width modulation; rotors; secondary cells; three-term control; PWM command; PWM-rpm-voltage; baseline PID controller; battery drainage; compensation control system; current battery voltage; model variation; online mass estimator; payload mass; pulse width modulation; quadrotor mass; subsystem compensates; Batteries; Equations; Mathematical model; Payloads; Propellers; Pulse width modulation; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Unmanned Aircraft Systems (ICUAS), 2014 International Conference on
  • Conference_Location
    Orlando, FL
  • Type

    conf

  • DOI
    10.1109/ICUAS.2014.6842339
  • Filename
    6842339