US 12,222,734 B2
Control apparatus, non-transitory computer readable medium, aircraft, system, and operating method of system
Shotaro Suzuki, Nagakute (JP)
Assigned to TOYOTA JIDOSHA KABUSHIKI KAISHA, Toyota (JP)
Filed by TOYOTA JIDOSHA KABUSHIKI KAISHA, Toyota (JP)
Filed on Oct. 17, 2022, as Appl. No. 18/047,083.
Claims priority of application No. 2021-170428 (JP), filed on Oct. 18, 2021.
Prior Publication US 2023/0121122 A1, Apr. 20, 2023
Int. Cl. G01D 1/10 (2006.01); B60L 58/12 (2019.01); B64D 27/24 (2006.01); G05D 1/00 (2006.01); H01M 10/42 (2006.01); H01M 10/44 (2006.01); H02J 7/00 (2006.01)
CPC G05D 1/106 (2019.05) [B60L 58/12 (2019.02); B64D 27/24 (2013.01); G05D 1/0016 (2013.01); H01M 10/425 (2013.01); H01M 10/44 (2013.01); H02J 7/00032 (2020.01); H02J 7/0048 (2020.01); H02J 7/00712 (2020.01); H02J 7/007188 (2020.01); G05D 1/0022 (2013.01); H01M 2220/20 (2013.01)] 20 Claims
OG exemplary drawing
 
1. A control apparatus comprising:
a memory storing information on power consumption for flight of an aircraft flying by an electric rotor; and
a controller configured to instruct the aircraft to fly on a flight path passing through a power supply facility based on a remaining charge of the aircraft and the power consumption according to flight conditions when the aircraft flies to a destination,
wherein the flight conditions include a total change in flight altitude based on information about an altitude required for the aircraft in each unit area.