Energetically Optimal Flapping Flight via a Fully Discrete Adjoint Method with Explicit Treatment of Flapping Frequency
Author:
Affiliation:
1. University of California, Berkeley
2. Lawrence Berkeley National Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-4412
Reference28 articles.
1. Flapping and flexible wings for biological and micro air vehicles
2. Simulation of Flow About Flapping Airfoils Using Finite Element Incompressible Flow Solver
3. Flapping Wing Aerodynamics: Progress and Challenges
4. Optimization of Flapping Airfoils For Maximum Thrust and Propulsive Efficiency
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1. Kinodynamic planning for an energy-efficient autonomous ornithopter;Computers & Industrial Engineering;2022-01
2. Energetically Optimal Flapping Wing Motions via Adjoint-Based Optimization and High-Order Discretizations;Frontiers in PDE-Constrained Optimization;2018
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