Ensuring Survivability of Spacecraft Attitude Control System at Failures in Flywheel Cluster

A method for ensuring the survivability of a spacecraft attitude control system with minimally redundant cluster of the flywheels and magnetic actuator at the faults of any reaction wheels are presented. The results of computer simulation were obtained and it was found if any two of the four fly...

Full description

Bibliographic Details
Main Authors: Sergey Somov, Tatyana Somova
Format: Article
Language:English
Published: Turkish Air Force Academy 2021-01-01
Series:Havacılık ve Uzay Teknolojileri Dergisi
Subjects:
Online Access:http://jast.hho.edu.tr/index.php/JAST/article/view/434