Abstract
The following paper presents of the use of the modified BLT method for the synthesis of the control system of the UAV. The small helicopter was the example of the UAV. This method was used for controlling the linear acceleration in the vertical axis and angular velocities around the UAV’s symmetry axes. The linearized multivariable model was used as the model of the UAV. The presented examples illustrate the correct operation of the modified BLT method in the lowest level of the UAV’s control system.
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Kuś, Z., Nawrat, A. (2016). The Application of the Modified BLT Method for the Synthesis of UAV’s Control System. In: Nawrat, A., Jędrasiak, K. (eds) Innovative Simulation Systems. Studies in Systems, Decision and Control, vol 33. Springer, Cham. https://doi.org/10.1007/978-3-319-21118-3_20
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DOI: https://doi.org/10.1007/978-3-319-21118-3_20
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