A new variant of the B-dot control for spacecraft magnetic detumbling-Reference-Cited by-同舟云学术

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A new variant of the B-dot control for spacecraft magnetic detumbling

Published:2020-06 Issue: Volume:171 Page:14-22
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Desouky Mohammed A.A.^ORCID,Abdelkhalik Ossama

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference45 articles.

1. Survey of worldwide pico-and nanosatellite missions, distributions and subsystem technology;Bouwmeester;Acta Astronaut.,2010

2. Magnetic spacecraft attitude control: a survey and some new results;Silani;Contr. Eng. Pract.,2004

3. Satellite attitude control using only magnetorquers;Wang,1998

4. Magnetic satellite detumbling: the b-dot algorithm revisited;Lovera;IEEE, Am. Contr. Conf. (ACC),2015

Cited by 9 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

1. Building a Better B-Dot: Fast Detumbling with Non-Monotonic Lyapunov Functions;2024 IEEE Aerospace Conference;2024-03-02

2. On-orbit performance analysis of spinning spacecraft magnetic control laws. Application to the UPMSat-2 mission;Measurement;2024-02

3. Orbital stabilization of dynamically elongated small satellite using active magnetic attitude control;Keldysh Institute Preprints;2024

4. Comparison of Feedback Three-Axis Magnetic Attitude Control Strategies;Aerospace;2023-11-21

5. Designing attitude controller for nano/pico satellites at detumbling mode using magnetic sensor and actuator;Journal of Physics: Conference Series;2023-11-01

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