Bhattacharya, RaktimBalas, Gary J.Kaya, M. AlpayPackard, Andy2008-06-112008-06-112002Bhattacharya, R., Balas, G. J., Kaya, M. A., and Packard, A. (2002). "Nonlinear Receding Horizon Control of an F-16 Aircraft." Journal of Guidance, Control, and Dynamics. 25(5), 924-931.https://hdl.handle.net/11299/37102Reprinted with permission of the American Institute of Aeronautics and Astronautics, Inc. See http://www.aiaa.org/content.cfm?pageid=2 for more information.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.en-USArticle