Auxiliary memory for Apollo guidance computer. Volume 2 - Appendices D and E Final report
Program listings and auxiliary core memory signal dictionary for Apollo guidance computer
SEARCH · Engineering Papers
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Program listings and auxiliary core memory signal dictionary for Apollo guidance computer
Venus flyby, Mars flyby, and Mars orbital mission to evaluate navigation and guidance systems for manned interplanetary spacecraft
Subsystems of Mariner Venus 67 spacecraft guidance and control system
Minimum fuel guidance for time-open rendezvous, orbit transfer, and orbit transfer with tangential nominal impulses
Evaluation technique to measure performance of strapdown guidance systems designed for unmanned interplanetary missions
Voyager spacecraft terminal guidance system analysis
Optical radar and tracker development for spacecraft automatic guidance during rendezvous
Technological problem areas in developing manned spacecraft navigation guidance and control systems
Unmanned spacecraft guidance and control technology for lunar and planetary exploration
Strapdown and gimbaled guidance and control systems for advanced unmanned spacecraft and launch vehicles
Navigation and guidance simulator for identifying performance capabilities of human operator during translunar or midcourse flight
Man computer roles and hardware requirements for navigation and guidance in deep space manned missions
Spacecraft guidance, trajectory analysis, and celestial mechanics - conference
Classification of spacecraft guidance modes according to approximations involved
Solution for minimum fuel guidance from hyperbolic to circular orbit
Guidance and control research - Josephson junction memory elements, frequency response of thin film thermal detectors, gallium selenide barrier gate, and photoconductor metal contacts
Adaptive orbital rendezvous guidance dynamic aspects valid for burn-coast-burn trajectories
Repetitive in-flight calculation of optimal rocket guidance using algorithm method for solving boundary value problem