Creates a linearized state-space model of a Boeing 707-321 aircraft at v=80 m/s (M = 0.26, Ga0 = -3 deg, alpha0 = 4 deg, kappa = 50 deg).
System inputs: (1) thrust and (2) elevator angle.
System outputs: (1) airspeed and (2) pitch angle.
Reference: R. Brockhaus: Flugregelung (Flight Control), Springer, 1994.
Package: control