Abstract
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 taken into account to give a bound on the predicted tracking error. The results of the algorithm are illustrated by applying the proposed algorithm to a simplified model of a trust vectored aircraft.
| Original language | English |
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| Pages | 1186-1191 |
| Number of pages | 6 |
| State | Published - 2001 |
| Event | 2001 IEEE International Symposium on Industrial Electronics Proceedings (ISIE 2001) - Pusan, Korea, Republic of Duration: 12 Jun 2001 → 16 Jun 2001 |
Conference
| Conference | 2001 IEEE International Symposium on Industrial Electronics Proceedings (ISIE 2001) |
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| Country/Territory | Korea, Republic of |
| City | Pusan |
| Period | 12/06/01 → 16/06/01 |