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公开(公告)号：US20240400217A1
公开(公告)日：2024-12-05
申请号：US18750785
申请日：2024-06-21
Applicant: Archer Aviation Inc.
Inventor： Jeffrey Mark BOSWORTH , Abhishek VAIDYA , Maicon SECCHI , Marcelo SANTOS
Abstract: The present disclosure relates generally to flight control of electric aircraft and other powered aerial vehicles. In one embodiment, an electrical system for an aircraft is disclosed, comprising: at least one processor configured to: receive pilot input indicating a commanded aircraft state, determine an aircraft thrust for achieving the commanded aircraft state, retrieve at least one propeller parameter associated with propeller speeds, wherein the propeller parameter is determined to reduce a structural vibratory response in the aircraft. The at least one processor is further configured to determine a respective command for each propeller of the aircraft to achieve the determined aircraft thrust based on the at least one propeller parameter and control each propeller of the aircraft based on the corresponding respective command.
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公开(公告)号：US20240400213A1
公开(公告)日：2024-12-05
申请号：US18614202
申请日：2024-03-22
Applicant: Archer Aviation Inc.
Inventor： Abhishek VAIDYA , Nathan Thomas DEPENBUSCH , Jenner Grey RICHARDS , Fernanda Aline Matta DE PAIVA
Abstract: Aspects of the present disclosure generally relate to systems and methods for flight control of aircrafts driven by electric propulsion systems and in other types of vehicles. In some embodiments, an aircraft is disclosed, comprising: at least one electric propulsion unit; at least one sensor configured to measure at least one aircraft condition; and at least one flight control computer configured to dynamically vary at least one torque command to the at least one electric propulsion unit based at least on the at least one aircraft condition; wherein the at least one electric propulsion unit is configured to generate thrust based on the at least one dynamically varied torque command.
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