Active model-based nonlinear system identification of quad tilt-rotor UAV with flight experiments-Reference-Cited by-同舟云学术

Active model-based nonlinear system identification of quad tilt-rotor UAV with flight experiments

Published:2022-07-27 Issue:8 Volume:65 Page:
ISSN:1674-733X
Container-title:Science China Information Sciences
language:en
Short-container-title:Sci. China Inf. Sci.

Author:

Liu Zhong,Theilliol Didier,He Yuqing,Gu Feng,Yang Liying,Han Jianda

Publisher

Springer Science and Business Media LLC

Subject

General Computer Science

Link

https://link.springer.com/content/pdf/10.1007/s11432-020-3074-5.pdf

Reference32 articles.

1. Liu Z, He Y Q, Yang L Y, et al. Control techniques of tilt rotor unmanned aerial vehicle systems: a review. Chin J Aeronaut, 2017, 30: 135–148

2. Ferguson S W. A mathematical model for real time flight simulation of a generic tilt-rotor aircraft. NASA CR-166536. 1988

3. Ye L, Zhang Y, Yang S, et al. Numerical simulation of aerodynamic interaction for a tilt rotor aircraft in helicopter mode. Chin J Aeronaut, 2016, 29: 843–854

4. Du S L, Wang C, Sun H J, et al. Numerical analysis of aerodynamic interference of rotor/fuselage in transition state of tilting four-rotor UAV. J Nanjing Univ Aeronaut Astronaut, 2018, 50: 179–185

5. Chen K, Shi Z W, Tong S X, et al. Aerodynamic interference test of quad tilt rotor aircraft in wind tunnel. Proc I Mech Eng Part G-J Aer Eng, 2019, 233: 5553–5566

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