Specifications

10 Design Case Studies
10-4
b =
rudder aileron
beta 0.0729 0
yaw -4.75 0.00775
roll 0.153 0.143
phi 0 0
c =
beta yaw roll phi
yaw 0 1 0 0
bank angle 0 0 0 1
d =
rudder aileron
yaw 0 0
bank angle 0 0
Continuous-time model.
The model has two inputs and two outputs. The units are radians for beta
(sideslip angle) and phi (bank angle) and radians/sec for yaw (yaw rate) and
roll (roll rate). The rudder and aileron deflections are in radians as well.
Compute the open-loop eigenvalues and plot them in the -plane.
damp(sys)
Eigenvalue Damping Freq. (rad/s)
-7.28e-003 1.00e+000 7.28e-003
-5.63e-001 1.00e+000 5.63e-001
-3.29e-002 + 9.47e-001i 3.48e-002 9.47e-001
-3.29e-002 - 9.47e-001i 3.48e-002 9.47e-001
s