Abstract
The probability of a malfunction in the operation of the onboard control system of an unmanned aerial vehicle under the influence of induced interference from a lightning discharge in the near zone is considered. The temporal shape and parameters of the induced interference are obtained on the basis of physical modeling. A technique for physical modeling and a test bed for physical experiments on a reduced scale were developed. An example of calculating the probability of failure in the operation of the onboard control system of an unmanned aerial vehicle under the influence of induced interference is given.
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Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2021, No. 3, pp. 180 - 186.
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Gizatullin, Z.M., Shleimovich, M.P. Analysis of Noise Immunity of the UAV Onboard Control System Based on Physical Modeling of Induced Interference. Russ. Aeronaut. 64, 554–561 (2021). https://doi.org/10.3103/S1068799821030259
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DOI: https://doi.org/10.3103/S1068799821030259