IDENTIFICATION AND SIMULATION EVALUATION OF A COMBAT HELICOPTER IN HOVER

Frequency-domain parameter identification techniques were used to deve lop a hover mathematical model of the AH-64 Apache helicopter from fli ght data. The unstable AH-64 bare-airframe characteristics, without a stability augmentation system, were parameterized in the conventional stability-derivative form. To improve the model's vertical response, a simple transfer-function model approximating the effects of dynamic i nflow was developed. The model, with and without stability augmentatio n, was then evaluated by AH-64 pilots in a moving-base simulation. It was the opinion of the pilots that the simulation was a satisfactory r epresentation of the aircraft for the tasks of interest. The principal negative comment was that height control was more difficult in the si mulation than in the aircraft.