Keywords :
Feedback linearization; flight control; nonlinear dynamic inversion; nonlinear systems; quadcopter; unmanned aerial vehicle; Aerial vehicle; Control schemes; Control strategies; Feedback linearisation; Flight control; Inversion control; Mathworks; Nonlinear dynamic inversion; Quadcopter; Unmanned aerial vehicle; Aerospace Engineering; Mechanical Engineering; Control and Optimization; Modeling and Simulation
Abstract :
[en] In this work, a flight control scheme based on incremental nonlinear dynamic inversion (INDI) is implemented within the Mathworks Simulink environment dedicated to the Parrot Mambo minidrone. This implementation is tested both in simulation and in real-life tests, and compared to the original cascade PID control structure. Trajectory tracking, robustness to modeling uncertainties and instrumentation issues are discussed. The resulting implementation can be used for educational purposes related to feedback linearization and the INDI controller in flight control applications.
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