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The design of a linear parameter varying (LPV) controller for the F-16 longitudinal axes over the entire è ight envelope, using a blending methodology that lets an LPV controller preserve regional optimal solutions over each parametersubsetand reducescomputationalcostsforsynthesizing anLPVcontroller,ispresented.Threeblending LPV controller synthesis methodologies are applied to control F-16 longitudinal axes. By the use of a function substitution method, a quasi-LPV model of the F-16 longitudinal axes is constructed from the nonlinear equations of motion over the entire è ight envelope, including nontrim regions, to facilitate synthesis of LPV controllers for the F-16 aircraft. The nonlinear simulations of theblended LPV controller show that the desired performance and robustness objectives are achieved across all altitude variations.

Blending Methodology of Linear Parameter Varying Control Synthesis of F-16 Aircraft System