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Precise laser gyroscope for autonomous inertial navigation
- Source :
- Quantum Electronics. 45:78-88
- Publication Year :
- 2015
- Publisher :
- IOP Publishing, 2015.
-
Abstract
- Requirements to gyroscopes of strapdown inertial navigation systems for aircraft application are formulated. The construction of a ring helium – neon laser designed for autonomous navigation is described. The processes that determine the laser service life and the relation between the random error of the angular velocity measurement and the surface relief features of the cavity mirrors are analysed. The results of modelling one of the promising approaches to processing the laser gyroscope signals are presented. (laser gyroscopes)
- Subjects :
- Physics
business.industry
Acoustics
Physics::Optics
chemistry.chemical_element
Statistical and Nonlinear Physics
Gyroscope
Angular velocity
Laser
Atomic and Molecular Physics, and Optics
Physics::Geophysics
Electronic, Optical and Magnetic Materials
law.invention
Computer Science::Robotics
Neon
Optics
chemistry
law
Inertial measurement unit
Random error
Ring laser gyroscope
Physics::Atomic Physics
Electrical and Electronic Engineering
business
Inertial navigation system
Subjects
Details
- ISSN :
- 14684799 and 10637818
- Volume :
- 45
- Database :
- OpenAIRE
- Journal :
- Quantum Electronics
- Accession number :
- edsair.doi...........9998cbd4badca5642b0d443c3396747c
- Full Text :
- https://doi.org/10.1070/qe2015v045n01abeh015420