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Function Reference: Boeing707

Function File: sys = Boeing707 ()

Creates a linearized state-space model of a Boeing 707-321 aircraft at \(v=80\,\frac{m}{s} (M = 0.26,\, G_{a0} = -3^{\circ},\, {\alpha}_0 = 4^{\circ},\, {\kappa}= 50^{\\circ}\)

System inputs:

  1. Thrust
  2. Elevator angle

System outputs:

  1. Airspeed
  2. Pitch angle

Reference: R. Brockhaus: Flugregelung (Flight Control), Springer, 1994.

Source Code: Boeing707