System for measuring force versus position of a flight...

Details System for measuring force versus position of a flight... System for measuring force versus position of a flight...

G - Physics

01

L

354/5

G01L 5/22 (2006.01) G01L 5/16 (2006.01) G09B 9/00 (2006.01)

Patent

CA 1315399

ABSTRACT OF THE DISCLOSURE A six-axis force transducer is mounted on the flight controller and provides three independent orthogonal linear force components of the applied force and three independent orthogonal torque components of the applied force. Change in position is measured by a motorized spool connected to a high resolution shaft encoder. A small diameter thread is wound around the spool via a mechanically driven threading device. The free end of the thread is connected to a fixed point in the cockpit. The output of the transducer and the shaft encoder are fed to a micro- processor which calculates net force, in accordance with well known formula, and net position, from calibration data.

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