IEEE 952-1997 PDF | Request Standard
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IEEE 952-1997

Axis Interferometric Fiber Optic Gyros

Standard by IEEE, 1997

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  • Language: English
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  • Language: English
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About This Item

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952-1997 is a technical standard for Axis Interferometric Fiber Optic Gyros, addressing the design and performance considerations associated with these navigation and sensing devices. In aerospace and transportation applications, it helps define a common reference for evaluating gyro behavior, consistency, and suitability for integration into electronic and control systems. For engineers, procurement teams, and test labs, the document supports clearer comparisons and more reliable specification of this specialized component.

952-1997 overview

This standard focuses on the axis interferometric fiber optic gyro as a component used in measurement and guidance-related systems. 952-1997 is relevant where precise rotational sensing is needed and where device characteristics must be understood in a controlled, repeatable way. By setting an identified technical framework, it can help align design expectations, qualification activities, and product selection for aerospace and related transportation equipment. It is especially useful when a consistent engineering reference is required.

Typical use cases

Axis interferometric fiber optic gyros are commonly considered in inertial sensing assemblies, navigation modules, and stabilization systems used in aerospace platforms and other transportation equipment. The standard may support integration work for flight-control electronics, attitude sensing, and test setups that depend on rotational measurement performance. It can also be useful during component sourcing, where engineers need to compare device capability, interface expectations, and suitability for a particular system architecture.

Why this standard matters

952-1997 matters because fiber optic gyro performance can affect system accuracy, stability, and overall confidence in guidance or control functions. A defined standard helps reduce ambiguity during design reviews, acceptance testing, and procurement, especially when multiple suppliers or configurations are involved. It may also support risk reduction by giving teams a shared basis for evaluating whether a gyro meets the intended technical and operational requirements in aerospace and transportation contexts.

  • Axis interferometric fiber optic gyros
  • Aerospace and transportation applications
  • Component performance and consistency
  • Design, test, and procurement reference
SKU: c15312b3ae96

  • Publication Date: 1997
  • Standard Status: Inactive
  • Publisher: IEEE
  • Subject: Aerospace; Components, Circuits, Devices and Systems; Transportation
  • Official IEEE: Doi link
  • New Version Available: 952 (2021)
  • Previous Version: 952 (2017)
  • This Version: 952 (1997)

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