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- W2045588750 abstract "SUMMARY Reliability of a satellite attitude control system depends on accurate detection of failures in its sensors. This paper presents an observer for robust detection and isolation of a class of failures in satellite attitude sensors. The proposed observer uses measurement of a three-axis gyro together with only one attitude sensor, and generates a residual signal which is sensitive to faults and is simultaneously robust against disturbance and noise. A nonlinear model of satellite kinematics is considered for design of the observer. The structure of the observer is in the form of a delayed continuous-time differential equation ensuring its robustness properties. A realistic simulation is provided to illustrate the performance of the proposed observer in the face of the faults occurring in a magnetometer, as the attitude sensor, and also the faults occurring in the gyro." @default.
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- W2045588750 date "2012-01-12" @default.
- W2045588750 modified "2023-09-27" @default.
- W2045588750 title "Robust detection and isolation of failures in satellite attitude sensors and gyro" @default.
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- W2045588750 doi "https://doi.org/10.1017/s0263574711001391" @default.
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