Deorbit kit demonstration mission
暂无分享，去创建一个
M. Tajmar | E. Lorenzini | A. Brunello | A. Valmorbida | G. Sarego | G. Sánchez-Arriaga | L. Tarabini Castellani | A. Ortega | K. Wätzig | L. Olivieri | C. Drobny | S. Shahsavani | S. Madrid | Jan-Philipp Wulfkuehler | S. García González | R. Nerger
[1] M. Tajmar,et al. A bare-photovoltaic tether for consumable-less and autonomous space propulsion and power generation , 2021 .
[2] Lorenzo Olivieri,et al. Deployment requirements for deorbiting electrodynamic tether technology , 2021, CEAS Space Journal.
[3] G. Sánchez-Arriaga,et al. The E.T.PACK project: Towards a fully passive and consumable-less deorbit kit based on low-work-function tether technology , 2020, Acta Astronautica.
[4] Hiroyuki Okamoto,et al. Review of KITE – Electrodynamic tether experiment on the H-II Transfer Vehicle , 2020 .
[5] M. Yu. Ovchinnikov,et al. Choosing control parameters for three axis magnetic stabilization in orbital frame , 2015 .
[6] Mahmut Reyhanoglu,et al. Three-axis magnetic attitude control algorithms for small satellites in the presence of noise , 2011, 2012 12th International Conference on Control, Automation and Systems.
[7] Edna Wisniewski,et al. Aalborg Universitet Linear Time Varying Approach to Satellite Attitude Control Using only Electromagnetic Actuation , 1997 .
[8] Eduardo Ahedo,et al. Bare wire anodes for electrodynamic tethers , 1993 .
[9] M. Pertile,et al. Deorbiting Performance of Electrodynamic Tethers to Mitigate Space Debris , 2022 .
[10] M. Tajmar,et al. Development Roadmap of a Deorbit Kit Based on Electrodynamic Tether , 2020 .
[11] W. J. Raitt,et al. The TSS-1R electrodynamic tether experiment: Scientific and technological results , 1999 .