A L1 Adaptive Control Scheme for UAV copyright Landing Using Nonlinear Dynamic Inversion
This paper presents a L1 adaptive controller augmenting a dynamic inversion controller for UAV (unmanned aerial vehicle) copyright landing.A three axis read more and a power compensator NDI (nonlinear dynamic inversion) controller serves as the baseline controller for this architecture.The inner-loop command inputs are roll-rate, pitch-rate, yaw-ra