Back to Search
Start Over
Vertically Optimal Close Formation Flight Control Based on Wingtip Vortex Structure
- Source :
- Journal of Aircraft. 57:964-973
- Publication Year :
- 2020
- Publisher :
- American Institute of Aeronautics and Astronautics (AIAA), 2020.
-
Abstract
- In this paper, aiming to drive the unmanned aerial vehicle (UAV) to the optimal position of the vertical plane in the close formation flight, a control method that is based on extended state observ...
- Subjects :
- Physics
020301 aerospace & aeronautics
Lift coefficient
business.industry
Structure (category theory)
Aerospace Engineering
Vertical plane
02 engineering and technology
01 natural sciences
Aspect ratio (image)
010305 fluids & plasmas
Computer Science::Multiagent Systems
Computer Science::Robotics
0203 mechanical engineering
Computer Science::Systems and Control
Position (vector)
0103 physical sciences
Horseshoe vortex
Wingtip vortices
Micro air vehicle
Aerospace engineering
business
Subjects
Details
- ISSN :
- 15333868
- Volume :
- 57
- Database :
- OpenAIRE
- Journal :
- Journal of Aircraft
- Accession number :
- edsair.doi...........2489b1c16a65ba7f405d654ba6781b33