2023
DOI: 10.1002/aisy.202200297
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Wind Defiant Morphing Drones

Abstract: Intense winds are a challenge for vertical take‐off and landing drones with wings. In particular, in the hovering regime, wings are sensitive to wind currents that can be detrimental to their operational and energetic performances. Tail‐sitters are particularly prone to those wind currents because their wings are perpendicular to the incoming wind during hovering. This wind generates a large amount of drag and can displace and destabilize the vehicle, possibly leading to catastrophic failures. Herein, our morp… Show more

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Cited by 6 publications
(6 citation statements)
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References 22 publications
(33 reference statements)
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“…In the nonlinear Equation ( 8) and ( 9), the terms including S represent the additional forces/moments produced by the CG shift as the wing sweeping, and the terms including first and second derivatives of static moment are the additional forces and moments produced by the velocity and acceleration of aircraft's CG shift in wing asymmetric sweeping progress. The aerodynamic model is introduced, and the forces and moments exert on the drone are as follows: (10) where g refers to the gravitational acceleration, P indicates the pull of propeller, L, D, and Y correspond to the lift, drag, and lateral force of the UAV, respectively. And l A , m A , and n A , respectively, stand for the roll, pitch, and yaw aerodynamic moment.…”
Section: Dynamic Modeling Of the Morphing Wing Dronementioning
confidence: 99%
See 3 more Smart Citations
“…In the nonlinear Equation ( 8) and ( 9), the terms including S represent the additional forces/moments produced by the CG shift as the wing sweeping, and the terms including first and second derivatives of static moment are the additional forces and moments produced by the velocity and acceleration of aircraft's CG shift in wing asymmetric sweeping progress. The aerodynamic model is introduced, and the forces and moments exert on the drone are as follows: (10) where g refers to the gravitational acceleration, P indicates the pull of propeller, L, D, and Y correspond to the lift, drag, and lateral force of the UAV, respectively. And l A , m A , and n A , respectively, stand for the roll, pitch, and yaw aerodynamic moment.…”
Section: Dynamic Modeling Of the Morphing Wing Dronementioning
confidence: 99%
“…[ 9 ] During crosswind or gusty conditions, a larger control margin can enhance the drone's ability to maintain attitude. [ 10 ] To make the winged UAV more flexible, researchers have explored the application of asymmetric wing morphing for roll control in drones, and some have even conducted flight tests on prototypes. [ 11 ] There are two types of roll control methods for existing morphing wing drones: 1) methods based on wing deformation alone, and 2) methods based on the cooperation of aerodynamic control surfaces and wing morphing.…”
Section: Introductionmentioning
confidence: 99%
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“…(2) Existing controllers either ignore wind effect in the environment (e.g., Ritz and D’Andrea (2017); Lustosa (2017)), or compensate the disturbance through incremental control updates from increased control error (e.g., Smeur et al (2020); Tal and Karaman (2022)), while our proposed approach incorporates wind effect by adjusting the reference trajectory (e.g., attitude) to maintain coordinated flight based on the differential flatness and then tracks the adjusted trajectory in real time. Given the considerable aerodynamic efficiency loss of tail-sitter in windy conditions (Vourtsis et al, 2023), our proposed feedforward strategy compensates the wind effect in a pre-emptive way before the control error actually accumulates. (3) Existing controllers (Ritz and D’Andrea, 2017; Tal and Karaman, 2022) simultaneously track trajectories and process singularities, while our work decouples singularities from the tracking controller, by the two-stage architecture.…”
Section: Related Workmentioning
confidence: 99%