Zobrazeno 1 - 10
of 1 102
pro vyhledávání: '"attitude control system"'
Publikováno v:
Mathematics, Vol 12, Iss 16, p 2569 (2024)
The problem of optimal synthesis of a nonlinear system’s control law parameters of satellite attitude control under constraints is considered. The maximum stability degree of a system is considered as an optimality criterion. The reaction wheels’
Externí odkaz:
https://doaj.org/article/47f57e5078854e328b393a69a5e2664d
Publikováno v:
Automation, Vol 4, Iss 3, Pp 246-262 (2023)
The reaction flywheel is a crucial operational component within a satellite’s attitude control system. Enhancing the performance of the reaction flywheel speed control system holds significant importance for satellite attitude control. In this pape
Externí odkaz:
https://doaj.org/article/678a2399d7ff44c7b3d04c679f49f0c7
Publikováno v:
مکانیک هوافضا, Vol 19, Iss 2, Pp 69-82 (2023)
In this paper, a satellite attitude control system with the reaction wheels based on suboptimal robust tube based model predictive control is designed. The satellite receives many external bounded disturbances in space. Due to the fact that disturban
Externí odkaz:
https://doaj.org/article/8af2b1f698a24471b1854ca9f6eb9525
Autor:
Liwei Hao, Yingchun Zhang
Publikováno v:
Aerospace, Vol 11, Iss 6, p 416 (2024)
This article explores novel in-orbit drag-free technology that can be utilized for deep space detection scientific missions. In this study, we considered a two-test-mass drag-free method and analyzed the design of the drag-free and attitude control s
Externí odkaz:
https://doaj.org/article/20ed5d852b734bb1ab296d081e8f8954
Autor:
Muhammad Faisal Shehzad, Aamer Bilal Asghar, Mujtaba Hussain Jaffery, Khazina Naveed, Zsolt Čonka
Publikováno v:
Heliyon, Vol 9, Iss 10, Pp e20434- (2023)
Prompt attitude stabilization is more challenging in Nano CubeSat due to its minimal capacity, weight, energy, and volume-constrained architecture. Fixed gain non-adaptive classical proportional integral derivative control methodology is ineffective
Externí odkaz:
https://doaj.org/article/2e5a0e81496e4b7eac9972bc85a394ad
Publikováno v:
Zhongguo Jianchuan Yanjiu, Vol 17, Iss 6, Pp 223-235 (2022)
ObjectiveIn order to improve the attitude control performance of a remote operated vehicle (ROV) in complex underwater environments, the attitude control of ROV with multi-motor coordinated propulsion is studied. MethodsFirst, for the structure and a
Externí odkaz:
https://doaj.org/article/e69249e085794a55bb8027154cea6482
Publikováno v:
Applied Sciences, Vol 14, Iss 7, p 2867 (2024)
The study of satellite performance evaluation can reveal the ability of satellite systems to fulfil corresponding tasks in the space environment, and provide information support for the resource allocation and mission scheduling of in-orbit satellite
Externí odkaz:
https://doaj.org/article/c77516cbb1eb4b5cbfffb1282ba6919e
Akademický článek
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Akademický článek
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Publikováno v:
Aircraft Engineering and Aerospace Technology, 2021, Vol. 93, Issue 7, pp. 1145-1155.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-10-2020-0224