ENSURING THE SURVIVABILITY OF SPACECRAFT CONTROL SYSTEM AT CRITICAL FAILURES OF REACTION WHEELS
2021 ◽
Vol 23
(2)
◽
pp. 66-74
Keyword(s):
A method for ensuring the survivability of the spacecraft attitude control system with a minimally redundant cluster of flywheels by General Electric scheme and a magnetic drive in the event of the flywheels' failures is presented. The results of computer simulation were obtained and it was found that in case of failure of any two flywheels, the Earth survey satellite retains the ability to scanning observation given targets.
2019 ◽
Vol 56
(1)
◽
pp. 158-170
◽
2019 ◽
Vol 17
(4)
◽
pp. 822-835
◽
2008 ◽
Vol 222
(2)
◽
pp. 139-152
◽
2007 ◽
Vol 1
(2)
◽
pp. 221-230
◽
1999 ◽
Vol 32
(2)
◽
pp. 8033-8038
◽