Simmonds Precision Products, Inc.

Sanat Kumar Choudhury

Rajendra S Kekan

Arthur M Berenbaum

Skanda Gopalakrishna

Rohin Hilloowala

Steven M Levy

A landing gear system includes a landing gear collar and a strut assembly supported by the landing gear collar. The strut assembly includes a piston that is adjustable between a fully extended position and a fully compress position. The landing gear system further includes a rotary encoder and a controller. The rotary encoder rotates in response adjusting the piston and to outputs a data value in response to its rotation. The controller is in signal communication with the rotary encoder and determines a stroke of the piston based on the data value output from the rotary encoder.

Configurable rotary encoder including two point inflight auto calibration and error adjustment

Provided are embodiments for techniques for monitoring components of a system, where the techniques include determining an operational status of one or more processing modules, wherein the one or more processing modules comprise one or more local memories, and configuring the one or more local memories with threshold values for configuration parameters for one or more components. The techniques also include sensing sensor data for the one or more components, determining the health status of the one or more components by comparing sensor data for the configuration parameters to the threshold values for the configuration parameters, and transmitting the sensor data and the health status of the one or more components to a central server for storing the sensor data and the health status.

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Karnataka, India

Sanat Kumar Choudhury