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Transition Flight Trajectory Optimization for a Flapping-Wing Micro Air Vehicle with Unsteady Vortex-Lattice Method
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Transition Flight Trajectory Optimization for a Flapping-Wing Micro Air Vehicle with Unsteady Vortex-Lattice Method
Category √
Sub-Category √
Aerospace
Year √
2022
Author √
Second
Keywords
Flapping
Flight Dynamics
Simulation
Optimization
Trajectory
UVLM
Control
Status √
Published
Files
Aerospace_2022_Transition Flight Trajectory Optimization for a Flapping-Wing Micro Air Vehicle with Unsteady Vortex-Lattice Method.pdf
URL
https://doi.org/10.3390/aerospace9110660
4 more properties
Citation
Lee, S.-G., Yang, H.-H., Addo-Akoto, R., and Han, J.-H., 2022, “Transition Flight Trajectory Optimization for a Flapping-Wing Micro Air Vehicle with Unsteady Vortex-Lattice Method,” Aerospace, 9(11): 660.
