Influence of control system algorithms on the maneuvering characteristics of the aircraft-Reference-Cited by-同舟云学术

Influence of control system algorithms on the maneuvering characteristics of the aircraft

Published:2022-01-16 Issue:1 Volume:5 Page:123-130
ISSN:2523-3947
Container-title:Aerospace Systems
language:en
Short-container-title:AS

Author:

Kiselev Mikhail,Levitsky Sergey,Shkurin Maxim

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Computers in Earth Sciences,Mechanical Engineering,Social Sciences (miscellaneous),Aerospace Engineering,Control and Systems Engineering

Link

https://link.springer.com/content/pdf/10.1007/s42401-021-00124-8.pdf

Reference19 articles.

1. Xin M (2014) Unified nonlinear optimal flight control and state estimation of highly maneuverable aircraft. Aerosp Sci Technol. https://doi.org/10.1016/j.ast.2014.05.001

2. Serebryansky S, Barabanov A (2020) To the question of multi-criteria optimization of aircraft components in order to optimize its life cycle. Adv Sci Technol Eng Syst J. https://doi.org/10.25046/aj050649

3. Kulchak AM, Kosyanchuk VV, Zybin EY (2018) Reconfiguration of integrated aircraft control system in case of actuator failures with regard to control constraints. Sci Bulle Mosc State Tech Univ GA. 21(6):65–78. https://doi.org/10.26467/2079-0619-2018-21-6-65-78

4. Mohamed M, Madhavan G (2020) Reduced order model-based flight control system for a flexible aircraft. IFAC-PapersOnLine. https://doi.org/10.1016/j.ifacol.2020.06.013

5. Aircraft Accident Investigation Report (2018) PT. Lion Airlines Boeing 737 (MAX)// PK-LQP TanjungKarawang, West Java, Republic of Indonesia 29 October 2018. National Transportation Safety Committee

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