Abstract
In this article, output tracking for a class of nonlinear non-minimum phase systems with output delay is considered. By applying the first-order Pade approximation technique to deal with the time-delay function, the original control problem is reduced to the output-tracking problem of a new non-minimum phase system without delay. The bounded tracking profiles of the unstable internal dynamics in the new system are generated by using the nonlinear inversion-based method, and a complete sliding mode control scheme is proposed to stabilise the output-tracking error as well as the internal dynamics. Moreover, the proposed control scheme is applied to solve the flight-path angle tracking problem of an F-16 jet fighter.
| Original language | English |
|---|---|
| Pages (from-to) | 529-538 |
| Number of pages | 10 |
| Journal | International Journal of Systems Science |
| Volume | 42 |
| Issue number | 3 |
| DOIs | |
| State | Published - Mar 2011 |
Keywords
- F-16 jet fighter
- non-minimum phase system
- nonlinear inversion-based method
- output delay
- sliding mode control
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