Abstract
The peculiarities of developing the control actuators on the basis of combined electromechanical modules are examined. A technique of calculating and designing the power contour of the control actuator for different purposes in the form of electromechanical module, is presented.
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Original Russian Text © V.V. Morozov, A.V. Zhdanov, 2016, published in Izvestiya VUZ, Aviatsionnaya Tekhnika, 2016, No. 1, pp. 109–115.
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Morozov, V.V., Zhdanov, A.V. Peculiarities of the control actuator development on the basis of combined electromechanical modules. Russ. Aeronaut. 59, 118–125 (2016). https://doi.org/10.3103/S1068799816010190
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DOI: https://doi.org/10.3103/S1068799816010190