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NASA NTRS · 19620007158

A Design Solution to the Spacecraft Look-Angle Problem

J N Wilson·G G Coyle
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Abstract

As the state of the art of the design of spacecraft has progressed, one of the difficult problems which has arisen is the positioning and articulating of spacecraft elements which must “see” in different directions without interference. Some of these elements are: solar panels or collectors, Sun sensors, communication antennas, star seekers, planet tracking and scanning devices, rocket motors, attitude-control jets, and scientific instruments. This Report presents a method of testing a spacecraft design to determine how well it satisfies these look-angle requirements. This method is applied to both simple and complex cases, and examples of its use are presented. A means of assessing spacecraft constraints on trajectories is discussed. The method was developed for the Mariner interplanetary spacecraft, but should be applicable to other cases.

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MARINER PROGRAMPROJECTIONSPACECRAFT INSTRUMENTATIONINSTRUMENT ORIENTATION

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J N Wilson, G G Coyle. 1962-08-06. A Design Solution to the Spacecraft Look-Angle Problem. https://ntrs.nasa.gov/citations/19620007158

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