Aerospace Instrument-Making Annotation << Back CHARACTERISTICS OF THE STUDY OF DYNAMICAL SYSTEMS UNDER TEST FLIGHT V.V. Bondartsev L.A. Baranov A.A. Bordukov Flight tests are comprehensive aeronautical engineering field experiments, during which the measurement of almost all parameters and measurements themselves can be attributed to dynamic measurements. At present, the study of dynamical systems with flight tests can identify several methods, including methods of recovery of dif-ferential equations from experimental data. To assess the dynamic properties of measuring devices, with the help of differential equations can be directed to a num-ber of tasks in the problem of metrological support in the preparation of equipment to full-scale experiments. The paper presents a method and a software implementa-tion of the recovery of the differential equation known transmitters on the transition function. Key words: differential equation, flight testing, metrology, dynamical systems, labview. Contacts: E-mail: mp.job@icloud.com Pp. 37-42.