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Aerospace Instrument-Making

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A new concept of uav’s aircraft-type landing control automation
V.M. Terentiev, D.A. Yurina, O.V. Mihailova

The aircraft-type landing problem of conventional-aerodynamic-design UAVs (Unmanned Air Vehicle) is considered. The synthesis of the structure and algorithms of a motion control automatic system during the landing is conducted. The given problem is solved by systems absolute-invariance theory methods. E-mail: kbpa@san.ru Рр.: 16-21

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