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IEEE 813 : 1988

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IEEE 813 : 1988

SPECIFICATION FORMAT GUIDE AND TEST PROCEDURE FOR TWO-DEGREE-OF-FREEDOM DYNAMICALLY TUNED GYROS

Institute of Electrical & Electronics Engineers

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Table of Contents

Part I - Specification format
1 Scope and references
1.1 Scope
1.2 References
2 Applicable documents
2.1 Specifications
2.2 Standards
2.3 Drawings
2.4 Bulletins
3 Requirements
3.1 Description
3.2 General requirements
3.3 Performance
3.4 Mechanical requirements
3.5 Electrical requirements
3.6 Environmental requirements
3.7 Reliability
4 Quality assurance provisions
4.1 Classification of tests
4.2 Acceptance tests
4.3 Qualification tests
4.4 Reliability tests
4.5 Test conditions and equipment
4.6 Test methods
4.7 Data submittal
5 Preparation for delivery
6 Notes
6.1 Intended use
6.2 Ordering data
6.3 Model equations
Part II - Test procedure
7 Scope
8 Description
8.1 Angular displacement sensing
8.2 Angular rate sensing
8.3 Model equation
9 Test conditions and test equipment
9.1 Standard test conditions
9.2 Standard operating and test equipment
10 Test procedures
10.1 Examination of product (mechanical)
10.2 Examination of product (electrical)
10.3 Leak test
10.4 Polarity
10.5 Operating temperature test series
10.6 Pickoff test series
10.7 Torquer test series
10.8 Rotor rotation detector
10.9 Spin motor test series
10.10 Axis alignment
10.11 Limit stop
10.12 Tuned speed
10.13 Dynamic time constant
10.14 Drift rate test series
10.15 Spring rate drift rate coefficients
10.16 Dynamic response test series
10.17 Output noise
10.18 Generated fields
10.19 Turn-on and warm-up times
10.20 Environmental test series
Figures
1 Closed-loop frequency response
2 DTG mechanical schematic and misalignment
         angles
3 Typical DTG outline drawing
4 Typical DTG electrical schematic
5 Pulse wave shape requirements
6 DTG electronic instrumentation
7 Vibration drift test orientations
8 Typical loop disturbance test diagram
Tables
1 Torquer current designations for multiposition
         drift rate test
2 Computation of drift rate coefficients from
         multiposition drift rate test
3 Environmental test series
Appendices
A Dynamically tuned gyro design features
B Typical DTG open-loop frequency response
C A guide to the operation of a dynamically
         tuned gyro (DTG)
Appendix Figures
B1 Typical DTG open-loop frequency response
C1 Simplified DTG model (free gyro) block diagram
C2 Block diagram showing effect of adding spring
         rates, damping and effective gimbal angular
         momentum to DTG
C3 Caged DTG model block diagram
C4 Caged DTG model block diagram showing cross-
         axis servo compensation
C5 Two-axis platform mode of operation block
         diagram

Abstract

Defines the requirements for a two-degree-of-freedom dynamically turned gyro (DTG) to be used as a sensor in a [strap-down, gimballed] [inertial navigation system, attitude reference unit,-] for use in [an aircraft, a missile, a spacecraft, -] application. The characteristics of the external capture electronics are considered where necessary to define gyro performance.

General Product Information

Document Type Standard
Status Current
Publisher Institute of Electrical & Electronics Engineers