ABSTRACT
The research an autonomous miniature flying robots has intensified considerably, thanks to the recent growth of civil and military interest in Unmanned Aerial vehicles (UAV). In this paper a simple control algorithm to stabilize the attitude of a quadrotor aircraft subjected to various disturbances is presented. First, we present a dynamic model of the quadrotor followed by simulation and implementation of a classical PID controller; the results were inconclusive and show the stability of the quadrotor for different disturbances. Secondly, we present the navigation and control technology embedded in a recently commercialized micro Unmanned Aerial Vehicle (UAV) AR.Drone. Test flight stabilization will be conducted on the AR.Drone, experimental results are discussed and interpreted.
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- B. Manohar, and All, "A Robust Environment for Simulation and Testing of Adaptive Control for Mini-UAVs", 2009 American Control Conference Hyatt Regency Riverfrant, ST, Louis, MO, USA, June 2009. Google ScholarDigital Library
Index Terms
- Control and stabilization applied to micro quadrotor AR.Drone
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