Research in electrically supported vacuum gyroscope. Volume 1 - Summary Final report
Intent, results, and recommendations of research program for Electrically Supported Vacuum Gyroscope /ESVG/
SEARCH · Search NASA
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.
Intent, results, and recommendations of research program for Electrically Supported Vacuum Gyroscope /ESVG/
Electric torque analysis as part of research on Electrically Supported Vacuum Gyroscope /ESVG/
Suspension factors analyzed as part of research on Electrically Supported Vacuum Gyroscope /ESVG/ for spacecraft
Error analysis to improve readout accuracy of Electrically Supported Vacuum Gyroscope /ESVG
Suboptimal compensation of gyroscopic coupling for inertia-wheel attitude control by mathematical techniques
Synchronous vibration absorbers using gyroscopic systems, noting antiresonance with Perissogyro
Advanced strapdown gyroscope for spacecraft inertial navigation units
Optimum stabilization of solid body rotary motion with aid of guided gyroscope
Fabrication of hemispherical opposed self-acting gas bearings for gyroscopes
Calculating drift of electrostatic gyroscopes due to rotor asphericity
Computer simulation of Apollo Telescope Mount to evaluate performance of control moment gyroscope system used for stabilization
Single degree of freedom, floated, intermediate accuracy, integrating gyroscope state of the art and design criteria for spacecraft control applications
Criteria for designing inertial gyroscope systems
Two degree of freedom gyroscopes stability with hydrodynamic grooved rotor bearings, describing parallel and conical whirling rotor oscillations
Stability characteristics of two degree of freedom gyroscope having hydrodynamic grooved journal rotor bearings, discussing frequency of self excited oscillation
Control moment gyroscopes for space base wobble damping and attitude control systems
General relativistic precession of gyroscope in inclined orbit
Gyroscopic control of spin rate or orientation of rigid bodies constrained to rotate about fixed axis