A power generation control system 70 according to the present embodiment includes power generation devices 40a and 40b configured to generate electrical power by using engines 44a and 44b based on a target power generation amount, and to supply the generated electrical power to a load (i.e., rotors 20 and 29), flight controllers 92a and 92b configured to decide a target power feed amount, which represents an electrical power amount to be supplied to the load, based on a state of the load, and control sections 91a and 91b configured to control the power generation devices by evaluating reliability of the target power generation amount, selecting a calculation method of the target power generation amount based on a result of the evaluation, and calculating the target power generation amount by using a target power feed amount decided by the flight controllers according to the calculation method.
POWER GENERATION CONTROL SYSTEM, POWER GENERATION CONTROL METHOD, AND AIRCRAFT
2023-09-28
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
POWER GENERATION CONTROL SYSTEM AND POWER GENERATION CONTROL METHOD
Europäisches Patentamt | 2017
|POWER GENERATION CONTROL SYSTEM AND POWER GENERATION CONTROL METHOD
Europäisches Patentamt | 2017
|Europäisches Patentamt | 2023
|Power generation control method, power generation control system, and vehicle
Europäisches Patentamt | 2022
|Europäisches Patentamt | 2022
|