MATLAB CONTROL SYSTEM TOOLBOX 9 Spécifications Page 188

  • Télécharger
  • Ajouter à mon manuel
  • Imprimer
  • Page
    / 591
  • Table des matières
  • MARQUE LIVRES
  • Noté. / 5. Basé sur avis des utilisateurs
Vue de la page 187
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
Vue de la page 187
1 2 ... 183 184 185 186 187 188 189 190 191 192 193 ... 590 591

Commentaires sur ces manuels

Pas de commentaire