I have a mathematical model of aerial vehicle. I have developed a estimation strategy to estimate the biasses in IMU sensors (gyroscope and accelerometer), and finally got some estimation results. The estimated bias waveform contain lot of transients, small steady state errors and finally divergence after some time. But they clearly give indication of change of level when a substantial fault is injected. I need to do fault detection (0 or 1), then how to set threshold (this is fully new for me). Thanks any help will be highly appreciated
I do not have any prior knowledge about thresholding , how to do fault detection etc
