Table 1 The initial states of aircraft.
From: Fixed-time angle of attack constrained control for aircraft considering dynamic icing process
States | Values |
|---|---|
Velocity V | 150 m/s |
Altitude h | 400 m |
Flight path angle \(\gamma\) | 0 |
Pitch angle \(\theta\) | 5\(^ \circ\) |
Angle of attack \(\alpha\) | 5 \(^ \circ\) |
Pitch rate Q | 0 |
