Miniaturization of flight deflection measurement system

Details Miniaturization of flight deflection measurement system Miniaturization of flight deflection measurement system

1988-09-30

1990-01-30

Ruehl, Charles A.

Measuring and testing

Wind tunnel: aerodynamic wing and propeller study

34082569, G01M 900

Patent

active

048965332

ABSTRACT:
A flight deflection measurement system including a hybrid microchip of a receiver/decoder. The hybrid microchip decoder is mounted piggyback on the miniaturized receiver and forms an integral unit therewith. The flight deflection measurement system employing the miniaturized receiver/decoder can be used in a wind tunnel. In particular, the miniaturized receiver/decoder can be employed in a spin measurement system due to its small size and can retain already established control surface actuation functions.

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