Reduced minimum configuration fiber optic gyro for land navigation applications (Reprinted from Fiber Optic Gyros: 20th Anniversary Conference Proceedings, 1996)

被引:6
|
作者
Emge, S
Bennett, S
Dyott, R
Brunner, J
Allen, D
机构
[1] Andrew Corporation, Orlando Park, IL
关键词
fiber optic gyroscope; minimum configuration; navigation; open-loop; Sagnac interferometers;
D O I
10.1080/01468039708202297
中图分类号
O43 [光学];
学科分类号
070207 ; 0803 ;
摘要
Further cost reduction of the fiber optic gyroscope is necessary in order to meet the economic requirements of land navigation system.s We have previously concentrated on the reduction of the number of splices and component improvements in the open-loop, minimum configuration. Now we eliminate nonessential components and splices. The source-detector coupler is not part of the Sagnac interferometer and serves solely to provide isolation between the broadband optical source and the photodetector. Many commercial laser diodes incorporate a back-facet photodetector to monitor laser intensity. The signal returned from the Sagnac interferometer traverses the laser, is received at this photodetector, and can be distinguished from the laser signal by the bias modulation. Configuring a gyro in this manner eliminates a directional coupler and the separate photodetector as well as up to three fiber splices in an all-fiber gyroscope. A production, open-loop, fiber optic gyroscope has been modified to demonstrate this principal. The gyroscope can be constructed with only two fiber splices and exhibits performance comparable to the conventional minimum configuration.
引用
收藏
页码:427 / 437
页数:11
相关论文
共 3 条
  • [1] Reduced minimum configuration fiber optic gyro for land navigation applications
    Emge, S
    Bennett, S
    Dyott, R
    Brunner, J
    Allen, D
    [J]. FIBER OPTIC GYROS: 20TH ANNIVERSARY CONFERENCE, 1996, 2837 : 106 - 112
  • [2] Reduced minimum configuration fiber optic gyro for land navigation applications
    Emge, S
    Bennett, S
    Dyott, R
    Brunner, J
    Allen, D
    [J]. IEEE AEROSPACE AND ELECTRONIC SYSTEMS MAGAZINE, 1997, 12 (04) : 18 - 21
  • [3] Reduced minimum configuration fiber optic gyro for land navigation applications
    Emge, S
    Bennett, S
    Dyott, R
    Brunner, J
    Allen, D
    [J]. IEEE 1996 POSITION LOCATION AND NAVIGATION SYMPOSIUM, 1996, : 38 - 41