TWI771941B

An on-vehicle aircraft control system includes a winding device provided on a landing platform, a connecting member connecting the winding device and an aircraft and wound up or drawn out by the winding device, and a controller controlling the winding device and the aircraft. Upon receipt of a landi...

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Bibliographische Detailangaben
Hauptverfasser:	ARINAGA, TSUYOSHI, HASHIGUCHI, HIRONOBU, YASUTAKE, AKIRA
Format:	Patent
Sprache:	chi
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS ELECTRIC COMMUNICATION TECHNIQUE ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GYROSCOPIC INSTRUMENTS HELICOPTERS MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS NAVIGATION PARACHUTES PERFORMING OPERATIONS PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS PICTORIAL COMMUNICATION, e.g. TELEVISION SIGNALLING SURVEYING TESTING TRAFFIC CONTROL SYSTEMS TRANSPORTING VEHICLES IN GENERAL VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISEPROVIDED FOR
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Beschreibung
Zusammenfassung:	An on-vehicle aircraft control system includes a winding device provided on a landing platform, a connecting member connecting the winding device and an aircraft and wound up or drawn out by the winding device, and a controller controlling the winding device and the aircraft. Upon receipt of a landing request to land the aircraft on the landing platform, the controller winds up the connecting member by the winding device and controls an attitude of the aircraft so as to land the aircraft with a photographing unit provided on the aircraft facing in a specified photographing direction determined in advance.