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Design of engine control system for small helicopter

Mechatronics 2013: Recent Technological and Scientific Advances (2014) 757-762
DOI: 10.1007/978-3-319-02294-9_95
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Abstract

This paper deals with integration of feedforward into turbo-shaft engine control algorithm and its influence on control quality. The control system provides fuel feeding, gas-generator speed control, power turbine speed control and operation limits of critical parameters. The achieved results are shown and described below. © Springer International Publishing Switzerland 2014.

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Ertl, L., & Jasansky, M. (2014). Design of engine control system for small helicopter. In Mechatronics 2013: Recent Technological and Scientific Advances (pp. 757–762). Springer Science and Business Media Deutschland GmbH. https://doi.org/10.1007/978-3-319-02294-9_95

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