Association of a manned space station and an unmanned observatory.
Manned orbiting space station operation in association with unmanned observatory, comparing gimbal mounted, free floating, tethered and firmly fixed modes
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Manned orbiting space station operation in association with unmanned observatory, comparing gimbal mounted, free floating, tethered and firmly fixed modes
Squeeze-film bearing is studied to develop a low-friction suspension for the output-axis gimbal of a single-degree-of-freedom gyroscope. Included are a review of pertinent literature, the theory of squeeze-film lubrication, and design elements.
Gimbaled spinmotor, gyro assembly, and gyro test results for gas bearing gyroscopes with high G and sterilization capability
Strapdown and gimbaled guidance and control systems for advanced unmanned spacecraft and launch vehicles
Gimballed star trackers application to satellite attitude control for simplified signal processing
Simulation techniques to remove gimbal bearing looseness effect on frequency response and cross axis coupling of Saturn control system S-4B stage
Strapdown and gimballed inertial navigation systems history, engineering progress and current developments
Optical gimballing apparatus directs narrow fields of view throughout solid angle approaching 4 pi steradians. Image rotation produced by scanning can be eliminated or altered by gear trains directly linked to the scanning drive assembly. It provides the basis for a binocular scanning capability.
Design, testing and final characteristics of OAO gimballed star tracker
Unstabilized astronaut, hand-held and integrated life support EVA maneuvering units tested in gimbaled six degree of freedom servo driven moving base simulator
Gimbaled nozzle and liquid injection thrust vector control requirements for solid rocket two stage launch vehicles
Reducing noise induced by turbulent windage torques within gimbal of fluid rotor gyroscope
Dual cockpit wide angle visual cue simulator design, discussing sky-earth-sun projector with four axis gimbal drive
Control moment gyro /CMG/ for spacecraft attitude control, determining optimal gimbal angle rate for desired torque
Three axis attitude ion thrust vector control mechanism for solar electric propulsion spacecraft, discussing gimbal and translation actuators, array and cabling
Stabilizing gyro utilizing re-circulated liquid hydrostatic gimbal bearing
Three stage motion restraining mechanism for restraining and damping three dimensional vibrational movement of gimballed package during launch of spacecraft