Optimizing energy consumption of Micro Aerial Vehicles is one of several problems that remains to be solved in the domain of UAVs. In a recent work, a novel quadrotor was introduced that was able, when possible, to roll on the ground thanks to a tilting propeller and caster wheels. In the following work, we build upon this idea with a trirotor helicopter where all the rotors are independently tilting. This grants our model a greater maneuverability both in flight and on the ground. We validate in this paper the flatness-based control approach by showing the ability of our UAV to follow arbitrary trajectories on the ground.


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    Titel :

    Ground control of a hybrid tricopter


    Beteiligte:


    Erscheinungsdatum :

    2015-06-01


    Format / Umfang :

    599633 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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