Aerodynamic Analysis, Dynamic Modeling, and Control of a Morphing Aircraft-Reference-Cited by-同舟云学术

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Aerodynamic Analysis, Dynamic Modeling, and Control of a Morphing Aircraft

Published:2019-09 Issue:5 Volume:32 Page:04019058
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Yan Binbin¹,Li Yong²,Dai Pei³^ORCID,Liu Shuangxi⁴

Affiliation:

1. Associate Professor, School of Astronautics, Northwestern Polytechnical Univ., Xi’an 710072, China.

2. Senior Engineer, Shanghai Electro-Mechanical Engineering Institute, Shanghai 201109, China.

3. Ph.D. Candidate, School of Astronautics, Northwestern Polytechnical Univ., Xi’an 710072, China (corresponding author). ORCID: .

4. Ph.D. Candidate, School of Astronautics, Northwestern Polytechnical Univ., Xi’an 710072, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001047

Reference19 articles.

1. Aircraft dynamic response to variable wing sweep geometry

2. Modeling and Control of an Aeroelastic Morphing Vehicle

3. A Review of Morphing Aircraft

4. Time-Varying Dynamics of a Micro Air Vehicle with Variable-Sweep Morphing

5. Flight Dynamics of a Morphing Aircraft Utilizing Independent Multiple-Joint Wing Sweep

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1. Recurrent neural network-based predefined time control for morphing aircraft with asymmetric time-varying constraints;Applied Mathematical Modelling;2024-11

2. Experimental Structural Design of a Novel Variable-Sweep Wing Based on a Four-Bar Planar Linkage;Journal of Aerospace Engineering;2024-11

3. Investigation of a Tube-Launched Unmanned Aerial Vehicle with a Variable-Sweep Wing;Drones;2024-09-10

4. A novel nonsingular fixed-time sliding mode control for morphing aircraft with actuator faults and saturation;Journal of the Franklin Institute;2024-09

5. Sliding Mode Flight Control Law Design Requirements for Oblique Wing Aircraft Based on Perturbation Theory;Aerospace;2024-05-06

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