Lunar Orbiter Spacecraft Guidance and Control System - An appraisal
Lunar Orbiter Spacecraft Guidance and Control, discussing design and flight results
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Lunar Orbiter Spacecraft Guidance and Control, discussing design and flight results
Low thrust station keeping guidance scheme for gravity gradient stabilized 24-hour satellite, solving equations of motion for near circular equatorial orbit
V/STOL aircraft automatic flight control, guidance and navigation by onboard computer, discussing mathematical model and simulation results
Guidance and navigation system design for automatic stationkeeping one earth orbiting vehicle with respect to other
Saturn 5 suboptimal continuous guidance design, eliminating discontinuous control encountered in SA-502 flight
Booster parameterized guidance algorithms investigated on basis of steering forms validity, discussing exoatmospheric ascent applications
Algorithm for trajectory analysis in closed loop terminal guidance of solar electrically thrusted interplanetary spacecraft
Manned spacecraft abort guidance and control problems, discussing various modes and emergency conditions
Guidance software package for digital flight control and landing system of CH-46C helicopter
Closed circuit television arc guidance adapter kit for computerized welding skate
Guidance and control considerations for advanced manned space missions
Guidance analyzer having suspended spacecraft simulating sphere for astronavigation
Guidance and control analysis and integration for interplanetary missions
Tape guidance system for multichannel digital recording system
Automatic closed circuit television arc guidance control for welding joints
Electrical and electromechanical trigonometric computation assembly and space vehicle guidance system for aligning perpendicular axes of two sets of three-axes coordinate references
Piloted simulator investigation of lightweight vehicles for emergency lunar escape to orbit with kinesthetic attitude control and simplified manual guidance
Development of procedures for midcourse and approach guidance of moon to earth trajectories based on optical angular measurements and onboard calculations