Aerodynamic Parameters Identification in Aircraft Longitudinal Motion
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In this book, the problem of aircraft parameters identification in conditions of measurement noises and influence analysis of input signal forms on the accuracy of aerodynamic parameters identification are discussed. All the signals involved into the process of identification are subjects to measurement noises, that is, measurement random errors normally distributed. The results of simulation are presented which show the relation between the noises standard deviations and the accuracy of identification.
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