Nonlinear receding horizon control of F-16 aircraft Academic Article

abstract

• In this paper 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 of the paper are i) Use of RHC to improve upon the performance of a LPV regulator. ii) Discussion on details of implementation such as control space formulation, tuning of RHC parameters, computation time and numerical properties of the algorithms. iii) Simulated response of nonlinear RHC and LPV regulator.

authors

• Bhattacharya, Raktim

published proceedings

• PROCEEDINGS OF THE 2001 AMERICAN CONTROL CONFERENCE, VOLS 1-6

author list (cited authors)

• Bhattacharya, R., Balas, G. J., Kaya, A., & Packard, A.

citation count

• 19

complete list of authors

• Bhattacharya, R||Balas, GJ||Kaya, A||Packard, A

publication date

• January 2001

publisher

• Institute of Electrical and Electronics Engineers (IEEE)  Publisher

published in

• Proceedings of the ... American Control Conference. American Control Conference  Journal

Digital Object Identifier (DOI)

• 10.1109/acc.2001.945598

start page

• 518

end page

• 522

volume

• 1

URL

• http%3A%2F%2Fdx.doi.org%2F10.1109%2Facc.2001.945598