Flywheel stabilized, magnetically torqued attitude control system for meteorological satellite study program
A 1964 NASA contractor engineering study on a flywheel-stabilized, magnetically torqued attitude control system for weather satellites, issued as a technical report for agency engineers. Line drawings show spacecraft assemblies with coils and gimbals, sight-line and mirror geometry diagrams, families of roll-angle curves against orbit fraction, and a photograph of a laboratory simulator rig.
