PROBLEM TO BE SOLVED: To make it possible to stabilize flight operation at the time of taking off and landing while enabling non-contact power supply to a flight vehicle.SOLUTION: A flight vehicle control device (drone control terminal 200) for controlling a flight vehicle (drone 100) comprises: a taking off and landing control part (control part 202) which indicates taking off and landing to the drone 100; and a power transmission control part 302 performs at least one of controls for instructing start of power transmission after landing of the drone 100 is terminated, and for indicating stop of power transmission before start of landing to a flight vehicle power supply device (power transmission side unit 300) which performs non-contact power supply for charging a battery 114 to the drone 100.SELECTED DRAWING: Figure 2

    【課題】飛行体への非接触な給電を可能にしつつ、離着陸の際の飛行動作を安定にする。【解決手段】飛行体(ドローン100)を制御する飛行体制御装置(ドローン制御端末200)は、ドローン100に離着陸を指示する離着陸制御部(制御部202)と、ドローン100にバッテリ114の充電用の非接触な給電をする飛行体給電装置(送電側ユニット300)に対して、ドローン100の着陸が完了した後に送電開始を指示し、または離陸開始前に送電停止を指示する制御の少なくとも一方を行う送電制御部302とを備える。【選択図】図2


    Access

    Download


    Export, share and cite



    Title :

    FLIGHT VEHICLE, FLIGHT VEHICLE POWER SUPPLY DEVICE, AND FLIGHT VEHICLE CONTROL DEVICE


    Additional title:

    飛行体、飛行体給電装置、および飛行体制御装置


    Contributors:

    Publication date :

    2017-04-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung





    FLIGHT VEHICLE SYSTEM, CONTROL DEVICE FOR FLIGHT VEHICLE, AND CONTROL PROGRAM FOR FLIGHT VEHICLE

    NAKA MASAHIRO / YAMAMOTO KENICHI | European Patent Office | 2020

    Free access

    FLIGHT VEHICLE CONTROL DEVICE AND FLIGHT VEHICLE CONTROL METHOD

    TAKAGI YUTAKA | European Patent Office | 2021

    Free access

    FLIGHT CONTROL DEVICE, FLIGHT CONTROL METHOD, FLIGHT VEHICLE

    IKOSHI SATOSHI / FUJIWARA DAIGO / SHIOKAWA TAKAYUKI et al. | European Patent Office | 2017

    Free access