FLIGHT CONTROL APPARATUS AND FLIGHT CONTROL METHOD

A flight control apparatus is a flight control apparatus for controlling a flight device operating by electric battery power supplied from a battery and includes a flight path acquisition unit that acquires a flight path, a flight control unit that causes the flight device to fly along the flight pa...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser:	TANAKA, Takaya
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CONTROLLING COSMONAUTICS ELECTRIC EQUIPMENT OR PROPULSION OF ELECTRICALLY-PROPELLEDVEHICLES ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES, IN GENERAL EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES PARACHUTES PERFORMING OPERATIONS PHYSICS REGULATING SIGNALLING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRAFFIC CONTROL SYSTEMS TRANSPORTING VEHICLES IN GENERAL
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Beschreibung
Zusammenfassung:	A flight control apparatus is a flight control apparatus for controlling a flight device operating by electric battery power supplied from a battery and includes a flight path acquisition unit that acquires a flight path, a flight control unit that causes the flight device to fly along the flight path, a battery remaining capacity acquisition unit that acquires a remaining capacity of the battery, and a specifying unit that specifies a charging facility for charging the battery, which corresponds to a position of the flight device, in which the flight control unit causes the flight device to fly to the specified charging facility and charge the battery, and then, causes the flight device to fly to the flight path, if the remaining capacity is less than or equal to a threshold value while the flight device flies along the flight path.