Hammer-head turn flight control of helicopters by using a thrust selection / desired attitude calculation based on a loading trajectory and a threshold-Reference-Cited by-同舟云学术

Hammer-head turn flight control of helicopters by using a thrust selection / desired attitude calculation based on a loading trajectory and a threshold

Published:2021 Issue:900 Volume:87 Page:21-00170-21-00170
ISSN:2187-9761
Container-title:Transactions of the JSME (in Japanese)
language:en
Short-container-title:

Author:

FUJIWARA Daigo¹

Affiliation:

1. Graduate School of Engineering, Chiba University

Publisher

Japan Society of Mechanical Engineers

Link

https://www.jstage.jst.go.jp/article/transjsme/87/900/87_21-00170/_pdf

Reference10 articles.

1. Abbeel, P., Coates, A., Quigley, M. and Ng, A. Y., An application of reinforcement learning to aerobatic helicopter flight, Advances in Neural Information Processing Systems 19: Proceedings of the 2006 Conference (2007), DOI: 10.7551/mitpress/7503.003.0006.

2. Bacon, B. J., Quaternion-based control architecture for determining controllability/maneuverability limits, Proceedings of the AIAA Guidance, Navigation, and Control Conference (2012), DOI: 10.2514/6.2012-5028.

3. Fujisaki, Y. and Ikeda, M., Synthesis of two-degree-of-freedom optimal servosystems, Transactions of the Society of Instrument and Control Engineers, Vol.27, No.8 (1991), pp.907–914, DOI: 10.9746/sicetr1965.27.907 (in Japanese).

4. Fujiwara, D. and Ota, M., Analytical modeling and verification experiments of small electric helicopters with stabilizers based on the blade-element approach, Transactions of the JSME (in Japanese), Vol.80, No.817 (2014), DOI: 10.1299/transjsme.2014tl0279.

5. Goodarzi, F. A., Lee, D. and Lee, T., Geometric adaptive tracking Control of a quadrotor UAV on SE(3) for agile maneuvers, ASME Journal of Dynamic Systems, Measurement and Control, Vol.137, No.9 (2015), Paper No. DS-14-1472, DOI: 10.1115/1.4030419.