Abstract
The functional diagram and algorithms for computing the altitude-speed parameters, the models of dynamic errors, and methods to ensure the accuracy of the system measuring channels based of the ion-mark sensor of primary information under deterministic and random influences are presented.
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Original Russian Text © V.M. Soldatkin, V.V. Soldatkin, A.V. Nikitin, V.Yu. Kornilov, 2018, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2018, No. 3, pp. 139–145.
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Soldatkin, V.M., Soldatkin, V.V., Nikitin, A.V. et al. Analyzing and Ensuring the Dynamic Accuracy of the Aircraft Air Data System with a Fixed Flush-Mounted Flow Receiver. Russ. Aeronaut. 61, 467–473 (2018). https://doi.org/10.3103/S1068799818030224
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DOI: https://doi.org/10.3103/S1068799818030224