Global Incremental Flight Control for Agile Maneuvering of a Tailsitter Flying Wing
Ezra Tal, Sertac Karaman

TL;DR
This paper introduces a novel global control law for tailsitter UAVs that enables accurate, agile maneuvering across the entire flight envelope, including uncoordinated sideslip flight, using differential flatness and incremental nonlinear dynamic inversion.
Contribution
It presents a new control approach combining differential flatness and INDI for robust, accurate trajectory tracking of tailsitter UAVs during complex maneuvers.
Findings
Demonstrated precise trajectory tracking in flight tests.
Achieved agile maneuvers including sideways flight and aggressive turns.
Controller robustness against aerodynamic model discrepancies.
Abstract
This paper proposes a novel control law for accurate tracking of agile trajectories using a tailsitter flying wing unmanned aerial vehicle (UAV) that transitions between vertical take-off and landing (VTOL) and forward flight. The global control formulation enables maneuvering throughout the flight envelope, including uncoordinated flight with sideslip. Differential flatness of the nonlinear tailsitter dynamics with a simplified aerodynamics model is shown. Using the flatness transform, the proposed controller incorporates tracking of the position reference along with its derivatives velocity, acceleration and jerk, as well as the yaw reference and yaw rate. The inclusion of jerk and yaw rate references through an angular velocity feedforward term improves tracking of trajectories with fast-changing accelerations. The controller does not depend on extensive aerodynamic modeling but…
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Taxonomy
TopicsAerospace and Aviation Technology · Adaptive Control of Nonlinear Systems · Advanced Vision and Imaging
