Deorbiting of Low Earth Orbit (LEO) microsatellites-Reference-Cited by-同舟云学术

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Deorbiting of Low Earth Orbit (LEO) microsatellites

Published:2009-08 Issue:2 Volume:55 Page:55-67
ISSN:1712-7998
Container-title:Canadian Aeronautics and Space Journal
language:en
Short-container-title:Can. Aeronaut. Space J.

Author:

Jablonski Alexander M,Scott Robert (Lauchie)

Publisher

Canadian Aeronautics and Space Institute

Subject

General Earth and Planetary Sciences,General Environmental Science

Cited by 15 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

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2. Optimal control scheme of space tethered system for space debris deorbit;Acta Astronautica;2019-12

3. Piecewise Parallel Optimal Algorithm;Optimization Algorithms - Examples;2018-09-05

4. Libration and transverse dynamic stability control of flexible bare electrodynamic tether systems in satellite deorbit;Aerospace Science and Technology;2016-02

5. Long-term dynamic modeling of tethered spacecraft using nodal position finite element method and symplectic integration;Celestial Mechanics and Dynamical Astronomy;2015-08-27

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