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公开(公告)号:US10962988B2
公开(公告)日:2021-03-30
申请号:US16177431
申请日:2018-11-01
Applicant: Bell Helicopter Textron Inc.
Inventor: Peter Carlton Mehl , Terrence Patrick Brehn , Robert Blyth , Brady G. Atkins
Abstract: A method of determining a center of gravity of an aircraft in flight by comparing actual control surface actuator displacements to expected control surface actuator displacements. And a method of fuel/load management based on an offset of the center of gravity from a preferred center of gravity and a handling qualities factor.