A Flight Measurement Method for Hinge Moment of Aircraft Control Surface with Redundant Actuation System in Active Mode

LI Jun; JIANG Xian

doi:10.3969/j.issn.2097-1915.2023.03.006

Home>Articles>A Flight Measurement Method for Hinge Moment of Aircraft Control Surface with Redundant Actuation System in Active Mode

DOI: 10.3969/j.issn.2097-1915.2023.03.006

A Flight Measurement Method for Hinge Moment of Aircraft Control Surface with Redundant Actuation System in Active Mode

LI Jun

JIANG Xian

Keywords：hinge moment of aircraft control surfaceflight measurementredundant actuation system in active modeforce-fightingoff-station load calibration teston-station load verification test

Publication Date：2023-06-25

Online Publishing Date：2025-08-15(First online date of this platform, not the publication date of the document)

Pages：7( 43-49 )

Journal of Air Force Engineering University

ISTICPKUCSCD

ISSN：2097-1915

Year, Vol.(Issue)：2023,24(3)