A system and various methods for determining a center of mass of an aircraft with a plurality of shock strut assemblies is illustrated. Multiple sensors, including a gas pressure sensor, and/or a position sensor, may be used to gather data and determine the center of mass of the aircraft. Various methods illustrated herein may evaluate the center of mass relative to a wheelbase axis and a wheel tread axis based on the gathered data.
AIRCRAFT WEIGHT AND CENTER OF MASS ESTIMATION SYSTEM
2022-01-13
Patent
Elektronische Ressource
Englisch
Aircraft Weight and Center of Mass Estimation System
SAE Technical Papers | 2016
|Aircraft Weight and Center of Mass Estimation System
British Library Conference Proceedings | 2016
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