Optical-inertia space sextant for an advanced space navigation system, phase B
Optical-inertia space sextant for advanced space navigation system
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Optical-inertia space sextant for advanced space navigation system
Guidance, control, and navigation for Apollo manned lunar landing mission - basic problems, onboard computation, safety aspects, and instrumentation
Apollo navigation and guidance - inertial measurement units and pulse torquing, optical measurements, guidance computer design, and attitude control systems.
Optical measurements and navigation problems during orbital and midcourse phases of Apollo space mission
Interplanetary trajectory computer program in Fortran for guidance and navigation studies
Transit satellite navigation system for use in ship positioning
Stabilization requirements for communications and navigation satellites
Computer evaluation of method for integrating orbital equations of motion for use in space navigation
Navigational accuracy of infrared acquisition and tracking system for Apollo reentry aircraft
Satellites for navigation aids for ships and transoceanic aircraft
Unmanned and manned satellites for communication and terrestrial navigation, noting future plans of NASA
Pilot acceptance factors in development of all- weather landing and SST navigation systems
Radar-updated inertial navigation of continuously- powered space vehicle during deboost phase of flight prior to lunar landing
Symbolic programming digital computer techniques, hardware interfacing and system errors in simulation of lunar midcourse guidance and navigation systems
Kalman filtering applied to error correction of inertial navigators
Analysis of sextant navigation measurements during lunar module rendezvous
Navigation and orbital performance of commercial communications satellites
Estimated man-machine requirement computations for space navigation and guidance