Abstract
In this paper, fault-tolerant active control of the rotational motion of the satellite has been applied. Satellite mathematical models are introduced and the non-traditional Kalman filter is designed with the presented control algorithms. Readjustment control procedure has been established taking into account the identified control distribution matrix. If there are three-axis reaction wheels on the satellite, the failure of one actuator, control setting is carried out using control distribution matrix diagnostics. Extended Kalman filter has been introduced to control the distribution estimation of matrix elements, so check back adjustment rule is applied by the fault tolerant attitude control.
Keywords
Control theory (sociology)
Kalman filter
Attitude control
Satellite
Control (management)
Actuator
Fault tolerance
Fault (geology)
Extended Kalman filter
Control engineering
Matrix (chemical analysis)
Computer science
Engineering
Artificial intelligence
Aerospace engineering
Distributed computing
Subject Areas
Inertial Sensor and Navigation
·Aerospace Engineering ·Physical Sciences
Space Satellite Systems and Control
·Aerospace Engineering ·Physical Sciences
Spacecraft Design and Technology
·Aerospace Engineering ·Physical Sciences