Advances in Inertial Navigation Systems and Components

摘要

Contents: Tuned Gyro Cost Reduction through a Novel Hinge Design; Optical Rotation Rate Sensors; A Nuclear Magnetic Resonance Gyro using Noble Gas Isotopes; Hamilton Standard Superjet TM Solid State Fluidic Rate Sensor; The Cactus Accelerometer; Inertial System Alignment and Calibration on a Moving Base; and Identification and Determination of Strapdown Error-Parameters by Laboratory Testing.