Modeling and Control for a Near-space Morphing Glide Aircraft

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/).

Download article (PDF)

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  -