Close-range air combat maneuver decision optimization method based on control parameterization

The invention discloses a close-range air combat maneuver decision optimization method based on control parameterization, and relates to the technical field of aircraft maneuver decision, comprising: defining a close-range air combat core factor dominant function; constructing a short-distance adaptive air combat dominant function according to the adaptive change weight coefficient and the short-distance air combat core factor dominant function; establishing an adaptive aircraft air combat maneuver decision optimal control problem; the adaptive aircraft air combat maneuvering decision optimal control problem is processed into a finite-dimension nonlinear programming problem which can be solved online; the maneuvering decision optimal control problem is approximated to be an online solvable and gradient solvable nonlinear programming problem; and solving an online solvable and gradient solvable nonlinear programming problem to obtain a close-range air combat maneuver decision based on control parameterization.