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In this paper, I reported that slanted rotor configuration can reduce pitching moment of quadrotor in horizontal flight. The quadrotor have rotors tiling to outerward. I confirmed decrease of pitching moment generation and decrease of rotor speed difference between rotors to cancel pitching moment in a wind tunnel experiment.

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This page is a summary of: Reduction of the head-up pitching moment of small quad-rotor unmanned aerial vehicles in uniform flow, International Journal of Micro Air Vehicles, December 2017, SAGE Publications,
DOI: 10.1177/1756829317745318.
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