Receding horizon control of an F-16 aircraft: A comparative study
by
T. Keviczky and G.J. Balas
in
IFAC Control Engineering Practice, vol. 14, no. 9, pp. 1023-1034, 2006.
Category: Journal Article
Keywords: Receding Horizon Control, Flight Control, Optimization
Click here to request an electronic copy of this paper.
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 an adaptive 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 adaptive 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.
This entry has been accessed 1463 times.