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NASA NTRS · 19930053881

Digital resolver for helicopter model blade motion analysis

Abstract

The paper reports the development and initial testing of a digital resolver to replace existing analog signal processing instrumentation. Radiometers, mounted directly on one of the fully articulated blades, are electrically connected through a slip ring to analog signal processing circuitry. The measured signals are periodic with azimuth angle and are resolved into harmonic components, with 0 deg over the tail. The periodic nature of the helicopter blade motion restricts the frequency content of each flapping and yaw signal to the fundamental and harmonics of the rotor rotational frequency. A minicomputer is employed to collect these data and then plot them graphically in real time. With this and other information generated by the instrumentation, a helicopter test pilot can then adjust the helicopter model's controls to achieve the desired aerodynamic test conditions.

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BibTeXRIS

Daniels, T. S., Berry, J. D., Park, S.. 1992-01-01. Digital resolver for helicopter model blade motion analysis. https://ntrs.nasa.gov/citations/19930053881

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