Model predictive tether-deployment control for precise landing of tethered reentry body

Author:

Kojima Hirohisa,Trivailo Pavel M.

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference40 articles.

1. Australian Space Academy, TERRESTRIAL ATMOSPHERE MODELLING, https://www.spaceacademy.net.au/watch/debris/atmosmod.htm (accessed May 20th, 2019).

2. Swing principle for deployment of a tether-assisted return mission of a re-entry capsule;Aslanov;Acta Astronaut.,2016

3. Tether-assisted re-entry capsule deorbiting from an elliptical orbit;Aslanov;Acta Astronaut.,2017

4. TiPS: results of a tethered satellite experiment;Barnds;Adv. Astronaut. Sci.,1997

5. Propellant-free control of tethered formation flight part 1: Linear control and experimentation;Chung;J. Guid. Control Dyn.,2008

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