Fault Detection of Aircraft System with Random Forest Algorithm and Similarity Measure

Table 1

Elevator trim value in longitudinal mode (normal mode elevator trim value: 5.752).

		Elevator stuck angle
		−10°	−5°	0°	+5°	+10°
Rudder stuck angle	−10°	—	—	−5.098	−10.008	—
	−5°	—	11.218	1.006	−9.150	—
	0°	—	10.173	5.796	−1.796	—
	5°	—	—	8.880	3.076	—
	10°	—	—	14.719	—	—
Elevator trim value (elevator stuck only)		12.640	10.173	5.796	−1.796	−9.898