FLIGHT CONTROL OF A VTOL AIR VEHICLE (QUADROTOR)

  • İ. Can DİKMEN
  • Aydemir ARISOY
  • Hakan TEMELTAŞ
Keywords: Quadrotor, Robust Control, PD, Back Stepping, Sliding Mode, Inverse Dynamic Control

Abstract

This study includes altitude stabilization, hovering control and attitude control of quadrotor.  Classically PD controller derived and applied to this system. Inverse dynamic control, feedback linearization control and sliding mode control methods have used to derive as nonlinear controllers. Linear and nonlinear control techniques applied to mathematical model as simulation and applied to quadrotor platform for experimental results. Derived control methods have been performed using computer simulations and compared the results according to this study objectives.

Published
2010-01-25
How to Cite
[1]
İ. C. DİKMEN, A. ARISOY, and H. TEMELTAŞ, “FLIGHT CONTROL OF A VTOL AIR VEHICLE (QUADROTOR)”, JAST, vol. 4, no. 3, pp. 33-40, Jan. 2010.
Section
Articles