The invention discloses a flight control system self-adaption parameter adjustment method. In the design process, the structure of a flight control system is fixed; and under the condition that flight envelope changes greatly, and by establishing constraint relation between unknown parameters of the flight control system and poles of a closed loop system, robust self-adaptive parameter adjustment of the flight control system is achieved. The method is characterized by, during the design process, to begin with, performing corresponding performance constraint based on flight qualities, such as bandwidth frequency, time delay, magnitude margin and phase margin, of an aircraft model, and establishing an area meeting flight performance requirements; and then obtaining design parameters, meeting area stabilization requirements, of the flight control system by utilizing the protection mapping theory, meanwhile, automatically generating a controller set meeting the requirements, and thus self-adaption parameter adjustment of the control system is achieved. More importantly, during the parameter adjustment process, not only a single parameter can be adjusted, but also coordinated and integrated design of multiparameters can be achieved, thereby meeting the requirement for multiobjective design parameter adjustment of the flight control system.