controlledJetEngine
differential equations modeling the dynamics of the Moore-Greitzer model of a jet engine
Contents
Syntax
f = controlledJetEngine(x,u,w)
Description
Dynamics equation for the controlled jet engine model.
Input Arguments
|
x |
system states x (dimension: [nx,1]) |
|
u |
control inputs u (dimension: [nu,1]) |
|
w |
disturbances w (dimension: [nw,1]) |
Output Arguments
|
f |
value of the dynamic function = time derivative of x |
See Also
References
[1] M. Krstic et al., "Nonlinear and Adaptive Control Design", John Wiley and Sons, 1995.
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