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Rotorcraft trajectory tracking by non linear inverse control

Abstract : The purpose of this communication is to investigate the usefulness of the non linear inverse 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 inverse approach is then proposed. A supervision level is introduced to take into account the actuator limitations.
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Submitted on : Tuesday, April 29, 2014 - 3:02:10 PM
Last modification on : Tuesday, October 19, 2021 - 11:17:58 PM
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  • HAL Id : hal-00938738, version 1


Antoine Drouin, Alexandre Carlos Brandao-Ramos, Thierry Miquel, Felix Mora-Camino. Rotorcraft trajectory tracking by non linear inverse control. DINCON 2007, 6th Brazilian Conference on Dynamics, Control and their Applications, May 2007, São José do Rio Preto, Brazil. pp xxxx. ⟨hal-00938738⟩



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