NASA NTRS · 19750018954
Apollo experience report guidance and control systems: Lunar module abort guidance system
Abstract
The history of a unique development program that produced an operational fixed guidance system of inertial quality is presented. Each phase of development, beginning with requirement definition and concluding with qualification and testing, is addressed, and developmental problems are emphasized. Software generation and mission operations are described, and specifications for the inertial reference unit are included, as are flight performance results. Significant program observations are noted.
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Kurten, P. M.. 1975-07-01. Apollo experience report guidance and control systems: Lunar module abort guidance system. https://ntrs.nasa.gov/citations/19750018954
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