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NASA NTRS ยท 19820011407

Attitude control subsystem study for the Land Mobile Satellite System Spacecraft

Abstract

This Attitude Control Subsystem study applies the generic antenna control technology to the specific requirements of the Land Mobile Satellite System mission and defines suitable attitude control subsystem designs for both the wrap/rib and hoop/column antenna configurations. The technology developments required to establish technology readiness by 1987 are also identified.

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BibTeXRIS

Tolivar, A. F.. 1982-03-01. Attitude control subsystem study for the Land Mobile Satellite System Spacecraft. https://ntrs.nasa.gov/citations/19820011407

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