Author:
Wang Siqi,Song Bifeng,He Lei
Reference19 articles.
1. Saeed AS, Younes AB, Islam S, Dias J, Seneviratne L, Cai G (2015) A review on the platform design, dynamic modeling and control of hybrid UAVs. In: Presented at the 2015 international conference on unmanned aircraft systems (ICUAS), pp 806–815. IEEE
http://doi.org/10.1109/icuas.2015.7152365
2. Rothhaar PM, Murphy PC, Bacon BJ, Gregory IM, Grauer JA, Busan RC, Croom MA (2014) NASA langley distributed propulsion VTOL tilt-wing aircraft testing, modelling, simulation, control, and flight test development. In: Presented at the 14th AIAA aviation technology, integration, and operations conference, 8 edn, vol 89, p 211. American Institute of Aeronautics and Astronautics, Reston, Virginia.
http://doi.org/10.2514/6.2014-2999
3. Tran AT, Sakamoto N, Sato M, Muraoka K (2017) Control augmentation system design for quad-tilt-wing unmanned aerial vehicle via robust output regulation method. IEEE Trans Aerosp Electron Syst 53(1):357–369.
https://doi.org/10.1109/TAES.2017.2650618
4. Muraoka K, Okada N, Kubo D, Sato M (2012) Transition flight of quad tilt wing VTOL UAV. In: Proceedings of 28th international congress aeronautical sciences, ICAS 2012-11.1.3, Brisbane, Australia
5. Sato M, Muraoka K (2016) Flight controller design for small quad tilt wing uav. J Jpn Soc Aeronaut Space Sci 64(1):79–82
Cited by
1 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献