Controlling the Speed Vector of an Aircraft-Reference-Cited by-同舟云学术

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Controlling the Speed Vector of an Aircraft

Published:2021-07 Issue:4 Volume:57 Page:331-337
ISSN:8756-6990
Container-title:Optoelectronics, Instrumentation and Data Processing
language:en
Short-container-title:Optoelectron.Instrument.Proc.

Author:

Zolotukhin Yu. N.,Kotov K. Yu.,Maltsev A. S.,Nesterov A. A.,Yan A. P.

Publisher

Allerton Press

Subject

Electrical and Electronic Engineering,Condensed Matter Physics,Instrumentation

Link

https://link.springer.com/content/pdf/10.3103/S8756699021040154.pdf

Reference9 articles.

1. Y. Wang, X. Zhu, Zh. Zhou, and Sh. Shao, ‘‘Landing control system design for a flying-wing aircraft based on ADRC,’’ in Intelligent Robotics and Applications. ICIRA 2014, Ed. by X. Zhang, H. Liu, Z. Chen, and N. Wang, Lecture Notes in Computer Science, vol. 8917 (Springer, Cham, 2014), pp. 340–351. https://doi.org/10.1007/978-3-319-13966-1_34

2. B. Newman and Th. Tran, ‘‘Back-stepping based flight path angle control algorithm for longitudinal dynamics,’’ in AIAA Guidance, Navigation, and Control Conf., Minneapolis, 2012 (AIAA, 2012), p. 4612. https://doi.org/10.2514/6.2012-4612

3. I. V. Miroshnik, V. O. Nikiforov, and A. L. Fradkov, Nonlinear and Adaptive Control of Complex Dynamic Systems (Nauka, St. Petersburg, 2000).

4. X. Wang, T. Mkhoyan, and R. de Breuker, ‘‘Nonlinear incremental control for flexible aircraft trajectory tracking and load alleviation,’’ in AIAA Scitech 2021 Forum, 2021, p. 0503. https://doi.org/10.2514/6.2021-0503

5. Th. Stastny and R. Siegwart, ‘‘Nonlinear model predictive guidance for fixed-wing UAVs using identified control augmented dynamics,’’ in Int. Conf. on Unmanned Aircraft Systems, Dallas, Texas, 2018 (IEEE, 2018), pp. 432–442. https://doi.org/10.1109/ICUAS.2018.8453377.

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