Vertically Optimal Close Formation Flight Control Based on Wingtip Vortex Structure
Author:
Affiliation:
1. Peking University, 100871 Beijing, People’s Republic of China
2. China Electronic Technology Group Corporation (CETC) Ocean Information Co., Ltd., 100041 Beijing, People’s Republic of China
Funder
Joint Fund of the Ministry of Education of China
National Natural Science Foundation of China
China Scholarship Council
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference25 articles.
1. Modeling of Aerodynamic Coupling Between Aircraft in Close Proximity
2. Nonlinear Control for Reconfiguration of Unmanned-Aerial-Vehicle Formation
3. Design, performance and modeling considerations for close formation flight
4. Formation Flight of Birds
5. Energy saving in flight formation
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. A Novel Use of Model Predictive Control with Extremum Seeking in Formation Flight;AIAA SCITECH 2024 Forum;2024-01-04
2. Reintroducing the Formation Flight Problem via Extremum Seeking Control;AIAA SCITECH 2024 Forum;2024-01-04
3. Extremum seeking control for UAV close formation flight via improved pigeon-inspired optimization;Science China Technological Sciences;2023-12-19
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