摘要：This paper presents a software to perform airplanes' flight test parameters identification. The software PIPEV is composed of a lot of subsystems developed to make: filtration of the results received from the flight records, choice of the most suitable teorical model; statistical identification of the model'. batic parameters, airplane's flight simulation comparing the results with the actual one, and creation and management of the aerodynamics data bank of the airplane that will be used in the manufacture of its flight simulator.
其他摘要：This paper presents a software to perform airplanes' flight test parameters identification. The software PIPEV is composed of a lot of subsystems developed to make: filtration of the results received from the flight records, choice of the most suitable teorical model, statistical identification of the model'. batic parameters, airplane's flight simulation comparing the results with the actual one, and creation and management of the aerodynamics data bank of the airplane that will be used in the manufacture of its flight simulator.
