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

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 t...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	KANO TOMOYOSHI, OGAWA TETSUSHI, YAMAGUCHI YUTAKA, NAKAMURA HARUYA, NISHIDA TOMOSUMI
Format:	Patent
Sprache:	eng ; jpn
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER CONTROLLING CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ELECTRICITY GENERATION GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HELICOPTERS PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES SYSTEMS FOR STORING ELECTRIC ENERGY TRANSPORTING
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	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