# controlledJetEngine

differential equations modeling the dynamics of the Moore-Greitzer model of a jet engine

## Contents

- Syntax
- Description
- Input Arguments
- Output Arguments
- See Also
- References

## 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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