Title :
Pointing grade fiber optic gyroscope
Author :
Killian, Kevin M.
Author_Institution :
AlliedSignal Guidance & Control Syst., Teterboro, NJ, USA
fDate :
7/1/1994 12:00:00 AM
Abstract :
Fiber optic gyroscopes (FOG) are solid-state rotation sensors that are appropriate for a wide variety of applications. In addition to becoming competitive with ring laser gyroscopes on new programs, FOGs are being manufactured to replace spinning wheel gyro technology in existing programs. The FOG brings with it the advantages of long life, high reliability, input axis stability, and low acceleration sensitivity. The AlliedSignal pointing grade fiber gyroscope was designed to replace a high-performance mechanical gyroscope currently made by AlliedSignal. Detailed passive thermal design, gyro assembly techniques, methods for rejecting light source intensity noise, and light source wavelength control are critical features that have been developed to produce a FOG with low noise, stable bias, and a stable and linear scale factor. Results of performance tests and error models indicate that these gyros have a capability for random walk of 0.0002 degrees//spl ne/ hour and bias stability of 0.001 degrees/hour.<>
Keywords :
aerospace instrumentation; attitude control; fibre optic sensors; gyroscopes; AlliedSignal; assembly; directional coupler; error models; light source intensity noise; light source wavelength control; low acceleration sensitivity; passive thermal design; performance tests; pointing grade fiber optic gyroscope; random walk; signal processing; solid-state rotation sensors; spacecraft attitude control; spinning wheel gyro technology; stability; Fiber lasers; Gyroscopes; Light sources; Manufacturing; Optical fiber sensors; Optical fibers; Optical sensors; Ring lasers; Solid state circuits; Stability;
Journal_Title :
Aerospace and Electronic Systems Magazine, IEEE