In-orbit performance of the OAO inertial reference unit

Computer Science – Performance

Scientific paper

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Inertial Reference Systems, Oao 3, Performance, Computer Programs, Data Reduction, Gyroscopes, Satellite Attitude Control

Scientific paper

Performance of the inertial reference unit (IRU) in the Orbiting Astronomical Observatory (OAO-C) is documented. The OAO and IRU are briefly described along with the data reduction programs used to calibrate the IRU in orbit. Application of gyros with good long-term drift stability to future spacecraft such as the Large Space Telescope and Earth Observatory Satellite is discussed.

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