Accurate modeling and robust hovering control for a quad-rotor VTOL aircraft

Jinhyun Kim, Min Sung Kang, Sangdeok Park

Research output: Contribution to journalArticlepeer-review

160 Scopus citations

Abstract

Quad-robot type (QRT) unmanned aerial vehicles (UAVs) have been developed for quick detection and observation of the circumstances under calamity environment such as indoor fire spots. The UAV is equipped with four propellers driven by each electric motor, an embedded controller, an Inertial Navigation System (INS) using three rate gyros and accelerometers, a CCD (Charge Coupled Device) camera with wireless communication transmitter for observation, and an ultrasonic range sensor for height control. Accurate modeling and robust flight control of QRT UAVs are mainly discussed in this work. Rigorous dynamic model of a QRT UAV is obtained both in the reference and body frame coordinate systems. A disturbance observer (DOB) based controller using the derived dynamic models is also proposed for robust hovering control. The control input induced by DOB is helpful to use simple equations of motion satisfying accurately derived dynamics. The developed hovering robot shows stable flying performances under the adoption of DOB and the vision based localization method. Although a model is incorrect, DOB method can design a controller by regarding the inaccurate part of the model and sensor noises as disturbances. The UAV can also avoid obstacles using eight IR (Infrared) and four ultrasonic range sensors. This kind of micro UAV can be widely used in various calamity observation fields without danger of human beings under harmful environment. The experimental results show the performance of the proposed control algorithm.

Original languageEnglish
Pages (from-to)9-26
Number of pages18
JournalJournal of Intelligent and Robotic Systems: Theory and Applications
Volume57
Issue number1-4
DOIs
StatePublished - Jan 2010

Keywords

  • Hovering control
  • QRT (quad-rotor type) UAV (unmanned aerial vehicle)
  • VTOL (vertical take-off and landing)

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