Advances in Inertial Navigation Systems and Components
Abstract
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1981
- Accession Number
- ADA101446
Entities
People
- Helmut Sorg
Organizations
- AGARD