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Receding horizon control of an F-16 aircraft: A comparative study
- Source :
-
Control Engineering Practice . Sep2006, Vol. 14 Issue 9, p1023-1033. 11p. - Publication Year :
- 2006
-
Abstract
- Abstract: A comparison between receding horizon control (RHC) approaches is presented for the longitudinal axis control of an F-16 aircraft. The results suggest that the flexibility provided by a scheduled RHC scheme based on flight condition-dependent linear prediction models is a necessary requirement for achieving good performance as opposed to a single LTI model-based method. The scheduled scheme offers an attractive alternative to a full nonlinear model-based RHC approach by trading off an acceptable degradation in performance to modest computational complexity and real-time implementability. [Copyright &y& Elsevier]
Details
- Language :
- English
- ISSN :
- 09670661
- Volume :
- 14
- Issue :
- 9
- Database :
- Academic Search Index
- Journal :
- Control Engineering Practice
- Publication Type :
- Academic Journal
- Accession number :
- 20524573
- Full Text :
- https://doi.org/10.1016/j.conengprac.2005.06.003