PROBLEM TO BE SOLVED: To provide a flight guidance system which enables an airframe unit to grasp its position without complicating the system and the process even in a location where the airframe unit has difficulty in receiving a navigation signal such as GPS.SOLUTION: An information acquisition part 32 provided at an airframe unit 11 is separated from the airframe unit 11 and reads information contained in an image 19 displayed on an instruction display device 12 provided on the ground or a floor. The airframe unit 11 acknowledges and specifies its flight position from a position of the instruction display device 12 and the read information displayed by the instruction display device 12. The airframe unit 11 continues flight on the basis of the acknowledged flight position.SELECTED DRAWING: Figure 1

    【課題】GPSなどの航法信号が受信しにくい場所でも、システムの複雑化および処理の煩雑化を招くことなく、機体ユニットが自らの位置を把握する飛行誘導システムを提供する。【解決手段】機体ユニット11に設けられている情報取得部32は、機体ユニット11から分離され、地上や床上に設けられている指示表示装置12に表示された画像19に含まれる情報を読み取る。機体ユニット11は、指示表示装置12の位置、および読み取られた指示表示装置12が表示する情報から自らの飛行位置を認識および特定する。機体ユニット11は、認識した飛行位置に基づいて、飛行を継続する。【選択図】図1


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    Title :

    FLIGHT GUIDANCE SYSTEM


    Additional title:

    飛行誘導システム


    Contributors:

    Publication date :

    2017-07-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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