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Differential flat control for rotorcraft trajectory tracking

Abstract : The purpose of this communication is to investigate the usefulness of the differential flatness control approach to solve the trajectory tracking problem for a four rotor aircraft. After introducing simplifying assumptions, the flight dynamics equations for the four rotor aircraft are considered. A trajectory tracking control structure based on a two layer non linear approach is then proposed. A supervision level is introduced to take into account the actuators limitations.
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Submitted on : Tuesday, April 29, 2014 - 3:17:58 PM
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  • HAL Id : hal-00938210, version 1


Nan Zhang, Geanina Andrei, Antoine Drouin, Felix Mora-Camino. Differential flat control for rotorcraft trajectory tracking. IMECS 2009, International Multiconference of Engineers and Computer Scientists, Mar 2009, Hong Kong, China. pp 1331-1336. ⟨hal-00938210⟩



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