Attitude Stabilization of Spacecraft in Very Low Earth Orbit by Center-Of-Mass Shifting

At very low orbital altitudes (≲450 km) the aerodynamic forces can become major attitude disturbances. Certain missions that would benefit from a very low operational altitude require stable attitudes. The use of internal shifting masses, actively shifting the location of the spacecraft center-of-ma...

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Bibliographic Details
Main Authors: Josep Virgili-Llop, Halis C. Polat, Marcello Romano
Format: Article
Language:English
Published: Frontiers Media S.A. 2019-02-01
Series:Frontiers in Robotics and AI
Subjects:
Online Access:https://www.frontiersin.org/article/10.3389/frobt.2019.00007/full