Design of infinite horizon LQR controller for discrete delay systems in satellite orbit control: A predictive controller and reduction method approach

Autor: Mohsen Khosravi, Hossein Azarinfar, Kiomars Sabzevari

Publikováno v: Heliyon, Vol 10, Iss 2, Pp e24265- (2024)

In the realm of satellite orbit control, powerful controller design plays a pivotal role in minimizing fuel consumption and ensuring orbit stability. This article introduces an advanced approach to the design of a Linear Quadratic Regulator (LQR) con

Externí odkaz: https://doaj.org/article/74fe17efcb3b4903a778eec39aa7ef2d

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Electron Emitter for small-size Electrodynamic Space Tether using MEMS Technology

Autor: Fleron, René A. W., Mogens Blanke

Publikováno v: Fleron, R A W & Blanke, M 2004, Electron Emitter for small-size Electrodynamic Space Tether using MEMS Technology . in Proceedings of the ESA Symposium on Small Spacecraft Systems . European Space Agency, La Rochelle, pp. 227-232, ESA Symposium on Small Spacecraft Systems, La Rochelle, France, Sept. 20-24, 01/01/2004 . < http://www.oersted.dtu.dk/publications/p.php?852 >
Technical University of Denmark Orbit

Adjustment of the orbit of a spacecraft using the forces created by an electro-dynamic space-tether has been shown as a theoretic possibility in recent literature. Practical implementation is being pursued for larger scale missions where a hot filame

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::435f24bb40d627de6377c8a61bedb8c0
https://orbit.dtu.dk/en/publications/3c293ab1-bf8b-4700-a975-302cc2d887aa