Nonlinear receding horizon control of an F-16 aircraft
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The application of receding horizon control (RHC) with the linear, parameter varying (LPV) design methodology to a high-fidelity, nonlinear F-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.
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
author list (cited authors)
Bhattacharya, R., Balas, G. J., Kaya, M. A., & Packard, A.
complete list of authors
Bhattacharya, R||Balas, GJ||Kaya, MA||Packard, A