MATEC Web Conf.
Volume 189, 20182018 2nd International Conference on Material Engineering and Advanced Manufacturing Technology (MEAMT 2018)
|Number of page(s)||9|
|Section||Cloud & Network|
|Published online||10 August 2018|
Dynamic modeling and control method of a new concept wing-disk aircraft
Naval Research Academy, Beijing, Chian
2 School of Computer Science and Technology, Tsinghua University, Beijing, China
* Corresponding author: firstname.lastname@example.org
The research aimed at a new layout wing-disk solar aircraft concept with several wings around the disc fuselage, select coordinates and variables adaptively for the new dynamic subject, and establish dynamic model, using blade element momentum theory and CFD value for correction. Design the flight control strategy and controller constraint relations, put forward the method of control allocation and manipulation, and use nonlinear dynamic inversion control method aimed at the transverse and longitudinal coupling, serious nonlinear characteristics, and adds integral element as a robust dynamic inverse control to deal with the poor performance of previous method, and simulate to validate the control design.
© The Authors, published by EDP Sciences, 2018
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