Constrained nonlinear receding horizon control and its application to a thrust vectored aircraft
This paper presents a receding horizon control method for input constrained nonlinear systems. The optimization procedure is based on predictions made by incremental models at points made by linearized incremental models eat points of a given seed trajectory and the effect of linearization error are...
| Autors principals: | , , , |
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| Format: | Conference item |
| Publicat: |
2001
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