A copy of this work was available on the public web and has been preserved in the Wayback Machine. The capture dates from 2020; you can also visit the original URL.
The file type is application/pdf
.
Spacecraft Attitude Fault-tolerant Control Based on Dynamic Control Distribution
2014
Sensors & Transducers
For spacecraft attitude control system, we consider the aircraft's control surface deflection position saturation and rate constraints. Based on the dynamic control allocation method, we put forward redistribution method in the event of actuator stuck and damage failure. Firstly, because of the system modeling error caused by uncertainty and external disturbance, under actuator stuck and damage failure, we put forward the attitude control system mathematical model of angular rate control. We
doaj:32cdf70b655d4f7298c77a93b6048387
fatcat:2pmme235efhxbeygwxvhbp3k74