Trajectory Inversion for a Rudderless Dual Vectored-Thrust Flying Wing
Trajectory Inversion for a Rudderless Dual Vectored-Thrust Flying Wing
This research proposes a trajectory generation method that jointly optimizes path geometry and timing for rudderless dual vectored-thrust flying wings. By using trajectory inversion to yield state and control histories satisfying coupled equations of motion, the approach balances curvature-induced acceleration against aerodynamic support to lower thrust-vectoring demand while retaining maneuver features. Representative looping and rolling sequences are tracked in closed-loop simulations, providing a basis for planning autonomous aerobatic maneuvers with such aircraft.
The study presents a trajectory generation method for rudderless dual vectored-thrust flying wings, optimizing path geometry and timing to balance curvature-induced acceleration against aerodynamic support; results are demonstrated in closed-loop simulations rather than physical deployment.
Source: arXiv Robotics — research abstracts · Read original article ↗
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closed-loop simulations. These results provide a basis for planning autonomous aerobatic maneuvers with rudderless vectored-thrust aircraft.
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arXiv:2611.10650v1 Announce Type: new Abstract: A rudderless dual vectored-thrust flying wing combines vertical takeoff and landing with efficient for- ward flight in a compact tailless configuration. Without aerodynamic control surfaces, vectored thrust couples translation and pitch control. Therefore, generating dy- namically compatible trajectories remains an open chal- lenge. To address this challenge, this study
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Source：arXiv Robotics — research abstracts · arxiv.org