For on-orbiting spacecraft, FTC and CA techniques are generally utilized to ensure the stability, reliability, autonomy and intelligence, and the percentage of successfully accomplished missions of the spacecraft ACS, especially in the presence of external disturbances, actuator constraints and faults.
Conclusions
Control Allocation for Spacecraft Under Actuator Faults ; Chapter : 10 ; 219-221
2021-03-14
3 pages
Article/Chapter (Book)
Electronic Resource
English
Springer Verlag | 2023
|Springer Verlag | 2022
|Wiley | 2022
|Springer Verlag | 2021
|Springer Verlag | 2019
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