METHOD OF CONTROLLING UNMANNED AIR VEHICLE

To enable an unmanned air vehicle to safely and efficiently fly while securing a flight distance and flight time.SOLUTION: An unmanned air vehicle 3 comprises: a flight control device; an annular ring body in which a part of a ring can be opened and closed; a current generating device; a ring openin...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	MAKABE KATSUHISA, TANIGUCHI MASAKAZU, OHARA HISAMASA, EMOTO KIYOSHI
Format:	Patent
Sprache:	eng ; jpn
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERATION HELICOPTERS PARACHUTES PERFORMING OPERATIONS SYSTEMS FOR STORING ELECTRIC ENERGY TRANSPORTING
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Schreiben Sie den ersten Kommentar!