This report investigates vibration induced attitude errors in strapdown inertial navigators."NASA CR-1396.""August 1969"--Cover.Includes bibliographical references (p. 175).This report investigates vibration induced attitude errors in strapdown inertial navigators.Prepared by the Analytic Sciences Corporation, Reading, Mass. for Electronics Research CenterMode of access: Internet
Cover title."September 1961."Space mechanics; Satellites; Stability and control.Includes bibliograph...
Prepared at Goddard Space Flight Center.Cover title.Includes bibliographical references (p. 15-16).M...
The ring laser gyro (RLG) dither axis will bend and exhibit errors due to the specific forces acting...
Systems analysis, design, and operating characteristics of strapdown gyroscopes for dynamic environm...
Error analysis for single degree of freedom integrating gyro, and figure of merit relating gyro erro...
Motion-induced errors in strapdown inertial navigation systems are discussed. The errors generated i...
Motion induced errors in a tuned, flexure-mounted strapdown gyro are investigated. Analytic expressi...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1962.In...
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1969. Sc.D.MIC...
This report investigates a radio/optical/strapdown inertial guidance system for unmanned space missi...
Impulsive or time-decaying disturbances of sufficient magnitude will cause a gravitygradient control...
International Telemetering Conference Proceedings / October 30-November 02, 1995 / Riviera Hotel, La...
This paper provides an overview of the primary strapdown inertial system computational elements and ...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994.In...
Proposed testing program for strapdown inertial system containing platform gyros and pendulous gyro
Cover title."September 1961."Space mechanics; Satellites; Stability and control.Includes bibliograph...
Prepared at Goddard Space Flight Center.Cover title.Includes bibliographical references (p. 15-16).M...
The ring laser gyro (RLG) dither axis will bend and exhibit errors due to the specific forces acting...
Systems analysis, design, and operating characteristics of strapdown gyroscopes for dynamic environm...
Error analysis for single degree of freedom integrating gyro, and figure of merit relating gyro erro...
Motion-induced errors in strapdown inertial navigation systems are discussed. The errors generated i...
Motion induced errors in a tuned, flexure-mounted strapdown gyro are investigated. Analytic expressi...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1962.In...
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1969. Sc.D.MIC...
This report investigates a radio/optical/strapdown inertial guidance system for unmanned space missi...
Impulsive or time-decaying disturbances of sufficient magnitude will cause a gravitygradient control...
International Telemetering Conference Proceedings / October 30-November 02, 1995 / Riviera Hotel, La...
This paper provides an overview of the primary strapdown inertial system computational elements and ...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994.In...
Proposed testing program for strapdown inertial system containing platform gyros and pendulous gyro
Cover title."September 1961."Space mechanics; Satellites; Stability and control.Includes bibliograph...
Prepared at Goddard Space Flight Center.Cover title.Includes bibliographical references (p. 15-16).M...
The ring laser gyro (RLG) dither axis will bend and exhibit errors due to the specific forces acting...