公开(公告)号：US20240336349A1

公开(公告)日：2024-10-10

申请号：US18628183

申请日：2024-04-05

申请人： Joby Aero, Inc.

发明人： Matthew Epperson ,  Thomas Victor Greenhill ,  Charles Graham Blair Horn

IPC分类号： B64C13/26 ,  B64C39/00 ,  B64C39/10 ,  G05D1/495 ,  G05D109/22

CPC分类号： B64C13/26 ,  G05D1/495 ,  B64C39/029 ,  B64C39/10 ,  G05D2109/22

摘要： A robust control method for an oblique flying wing aircraft includes computing an angular velocity error between a reference angular velocity and an actual angular velocity and computing a moment command with an angular velocity controller based at least in part on the angular velocity error. The angular velocity controller decouples two or more of a yaw rate axis, a pitch rate axis, and a roll rate axis of the asymmetric aircraft for the moment command.