Nonlinear receding horizon control of the F-16 aircraft
by
R. Bhattacharya, G.J. Balas, M.A. Kaya and A.K. Packard
in
AIAA Journal of Guidance, Dynamics and Control, vol. 25, no. 5, pp. 924-931, 2002.
Category: Journal Article
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Abstract:
The applicationof receding horizon control (RHC) with the linear, parameter varying(LPV) design methodology to a high-Ž delity, nonlinearF-16 aircraft model is demonstrated. The highlights are 1) use of RHC to improve upon the performance of a LPV regulator; 2) discussion on details of implementation such as control space formulation, tuning of RHC parameters, computation time and numerical properties of the algorithms; and 3) simulated response of nonlinear RHC and LPV regulator.
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