Accession Number:

ADA101446

Title:

Advances in Inertial Navigation Systems and Components

Descriptive Note:

Corporate Author:

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE)

Personal Author(s):

Report Date:

1981-04-01

Pagination or Media Count:

142.0

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.

Subject Categories:

  • Navigation and Guidance

Distribution Statement:

APPROVED FOR PUBLIC RELEASE