FDIA System for Sensors of the Aero-Engine Control System Based on the Immune Fusion Kalman Filter

Table 7

Thrust control expectation schedule.

Simulation time period (s)	Thrust expectation
0–15	Maintain 12,000 N
15–17	Linear change from 12000 N to 21000 N
17–30	Maintain 21,000 N
30–32	Linear change from 21000 N to 30000 N
32–47	Maintain 30,000 N
47–49	Linear change from 30000 N to 35000 N
49–62	Maintain 35,000 N
62–64	Linear change from 35000 N to 12000 N
64–80	Maintain 12,000 N