Modeling and Control for a Near-space Morphing Glide Aircraft
Authors
Tie Biao Chen, Min Gong, Chen Xi Wang, Lei Zhang, Bin Bai
Corresponding Author
Tie Biao Chen
Available Online September 2018.
- DOI
- 10.2991/iceep-18.2018.322How to use a DOI?
- Keywords
- near-space glide aircraft; morphing aircraft; auto disturbance rejection controller
- Abstract
According to the morphing requirements, this article proposes a morphing glide aircraft with high environmental adaptability. Based on Kane’s Method, six degree-of freedom dynamic model is built. The automatic disturbance rejection control technology is adopted to realize stability control of longitudinal model of MGA, that provides a reference for the control technology research of morphing aircraft.
- Copyright
- © 2018, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Tie Biao Chen AU - Min Gong AU - Chen Xi Wang AU - Lei Zhang AU - Bin Bai PY - 2018/09 DA - 2018/09 TI - Modeling and Control for a Near-space Morphing Glide Aircraft BT - Proceedings of the 2018 7th International Conference on Energy and Environmental Protection (ICEEP 2018) PB - Atlantis Press SP - 1769 EP - 1778 SN - 2352-5401 UR - https://doi.org/10.2991/iceep-18.2018.322 DO - 10.2991/iceep-18.2018.322 ID - Chen2018/09 ER -