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Control-Oriented Modeling of Coupled Electromechanical-Aeroelastic Dynamics for Flapping-Wing Vehicles
- Source :
- Journal of Guidance, Control, and Dynamics. 40:1664-1679
- Publication Year :
- 2017
- Publisher :
- American Institute of Aeronautics and Astronautics (AIAA), 2017.
-
Abstract
- A computationally tractable nonlinear aeroelastic model of a bioinspired flapping-wing micro air vehicle, which includes motor dynamics and is suitable for control evaluation, is developed in this ...
- Subjects :
- 020301 aerospace & aeronautics
Computer science
Applied Mathematics
Dynamics (mechanics)
Condensation
Aerospace Engineering
02 engineering and technology
Aeroelasticity
01 natural sciences
Finite element method
010305 fluids & plasmas
Flapping wing
Nonlinear system
0203 mechanical engineering
Control oriented
Space and Planetary Science
Control and Systems Engineering
Control theory
0103 physical sciences
Micro air vehicle
Electrical and Electronic Engineering
Subjects
Details
- ISSN :
- 15333884 and 07315090
- Volume :
- 40
- Database :
- OpenAIRE
- Journal :
- Journal of Guidance, Control, and Dynamics
- Accession number :
- edsair.doi...........b294683c6c12c566505a11038e2e02c2