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NASA NTRS · 19670053266

Control moment gyro development and test.

Fontana, A.·Keckler, C. R.

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Abstract

Hardware characteristics of control moment gyro /CMG/, determining nonlinearity effects on performance by simulation

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APOLLO SPACECRAFT DIRECTIONAL CONTROL CONTROL SYSTEM NONLINEAR SYSTEM ATTITUDE GYRO HARDWARE

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Fontana, A., Keckler, C. R.. 1967-01-01. Control moment gyro development and test.. https://ntrs.nasa.gov/citations/19670053266

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