Results of studies on a twin-gyro attitude- control system for space vehicles
Twin gyroscopic control system for three orthogonal axes of space vehicle attitude control
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Twin gyroscopic control system for three orthogonal axes of space vehicle attitude control
Dual field optical tracking system and television camera chain combined with two gyroscopes to form space navigation sextants
Miniature electrically suspended gyroscope for spacecraft attitude reference system
Hydrostatic pressurized gas lubricated journal and thrust bearings for gyroscope gimbal bearings - static and dynamic load and flow analysis
Fluid tube gyroscope and signal preamplifier
Viscous damping and gyroscopic effects on destabilization in linear system subjected to conservative forces
Gyroscopic drift and Markov process research in inertial guidance system components study
Time dependency of spherical squeeze-film bearing for use in suspension of precision gyroscope output
Statistical analysis of gyroscopic drift rate data for computer simulation of inertial navigator output error
Navigation and guidance principles and requirements - component technology, gyroscope application, inertial systems, specific force receivers, and geometrical aspects
Gyroscope system for inertial experiment pointing and attitude control of manned spacecraft
Density of six niobium spheres which are intended for use as rotors in superconducting gyroscope
Solar paddle and gyroscopic mechanism used for active and passive satellite attitude control for non-spinning spacecraft
Compatibility test data on strapdown electrically suspended gyroscope
Ceramics tested for use in hydrodynamic gyroscope gas bearings
Electrical breakdown in ultrahigh vacuum studied for electrostatic gyroscope development
Passive damping method for aligning instantaneous spin, symmetry, and angular momentum axes of solid axisymmetric almost spherical satellite gyroscope