Spacecraft Antenna Pointing

G E Fleischer

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NASA NTRS · 19670002775

Spacecraft Antenna Pointing

G E Fleischer

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Abstract

In examining the characteristic inaccuracies of a pre-programmed high-gain antenna pointing system, the effects of spacecraft attitude errors, as embodied in pitch, yaw and roll limit cycle activity, are of major concern. If the pointing accuracy requirements for a particular mission allow the use of a single degree of freedom pointing system, it is doubtful whether a method of correcting antenna position for spacecraft attitude errors would be worthwhile. This is because the pointing error due to fitting a plane curve to a three-dimensional trajectory would probably be at least as large as the additional pointing errors due to attitude drift within the deadbands. Further, trying to correct pointing for pitch, yaw, and roll drifts by adjusting a single hinge angle is relatively ineffective.

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G E Fleischer. 1966-08-31. Spacecraft Antenna Pointing. https://ntrs.nasa.gov/citations/19670002775

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