Aircraft landing gear longitudinal force control

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United States of America Patent

PATENT NO 9845148
SERIAL NO

14443282

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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An aircraft landing gear longitudinal force control system for an aircraft having landing gears with braking and/or driving wheel(s). The system includes an error-based force controller having feedback for minimising any error between the demanded force and the actual force achieved by the force control system. The feedback may be derived from force sensors on the landing gear for direct measurement of the landing gear longitudinal force. The force control system may include an aircraft level landing gear total force controller and/or a landing gear level force controller for each actuated landing gear.

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Patent Owner(s)

  • AIRBUS OPERATIONS LIMITED;AIRBUS OPERATIONS SAS

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Damiani, Andrea Bristol, GB 6 20
Gama-Valdez, Miguel Angel Bristol, GB 2 12
Romana, Louis-Emmanuel Toulouse, FR 11 39

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