Abstract
The paper considers the indirect measurement of disturbance based on the output parameters of the control object using its mathematical model and the disturbance compensation in order to improve the automatic control system noise resistance. The method proposed is applied to aircraft attitude motion control systems. The issues of such systems synthesis are considered. Modeling results are given.
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Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2020, No. 4, pp. 65 - 71.
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Petunin, V.I., Neugodnikova, L.M. Method of Improving the Noise Resistance of Automatic Control Systems. Russ. Aeronaut. 63, 627–634 (2020). https://doi.org/10.3103/S1068799820040091
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DOI: https://doi.org/10.3103/S1068799820040091