Flight Dynamics Modeling and Control of a Novel Catapult Launched Tandem-Wing Micro Aerial Vehicle With Variable Sweep
- DOI
- 10.1109/access.2018.2858293
- Published
- 2018
- Container
- IEEE Access
- Publisher
- Institute of Electrical and Electronics Engineers (IEEE)
- Open access
- unknown
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Cite this work
BibTeX
@article{allodium:10.1109/access.2018.2858293,
title = {Flight Dynamics Modeling and Control of a Novel Catapult Launched Tandem-Wing Micro Aerial Vehicle With Variable Sweep},
author = {Liang Gao and Hongzhe Jin and Jie Zhao and Hegao Cai and Yanhe Zhu},
year = {2018},
journal = {IEEE Access},
doi = {10.1109/access.2018.2858293},
url = {https://doi.org/10.1109/access.2018.2858293}
}RIS
TY - JOUR TI - Flight Dynamics Modeling and Control of a Novel Catapult Launched Tandem-Wing Micro Aerial Vehicle With Variable Sweep AU - Liang Gao AU - Hongzhe Jin AU - Jie Zhao AU - Hegao Cai AU - Yanhe Zhu PY - 2018 JO - IEEE Access DO - 10.1109/access.2018.2858293 UR - https://doi.org/10.1109/access.2018.2858293 ER -
APA
Gao, L., Jin, H., Zhao, J., Cai, H., & Zhu, Y. (2018). Flight Dynamics Modeling and Control of a Novel Catapult Launched Tandem-Wing Micro Aerial Vehicle With Variable Sweep. IEEE Access. https://doi.org/10.1109/access.2018.2858293
Source records
- crossref · retrieved 2026-09-26T09:09:15.402Z