IEEE 529 : 1980

Table of Contents

User's cross reference
Part I - Specification format
1 Scope
3.2.2 Definitions
3.3.9.2.1 Command rate scale factor errors
3.3.9.2.2 Command rate scale factor sensitivities
3.3.18 Output noise
3.3.22.5 Torquer time constant
3.3.24 Anisoinertia drift rate coefficient
3.3.25 Cross-coupling drift rate
3.3.25.1 Non-oscillatory
3.3.25.2 Spin-input rectification
3.3.25.3 Spin-output rectification
3.3.26 Torquer current rectification drift rate
3.3.27 Rate hysteresis error
3.3.28 Output axis rate error
3.6.4.1 Vibration
3.6.4.1.1 Linear
3.6.4.1.2 Angular
4.6 Test methods
4.5.18.5.1 Vibration, linear
4.6.18.5.2 Vibration, angular
6.3 Model equation
Part II - Test procedures
9.1.1.4 Vibration
9.1.1.4.1 Linear
9.1.1.4.2 Angular
9.2.2 Standard operating equipment
10.7 Torquer test series
10.7.1 Purpose
10.7.2 Test equipment
10.7.3 Test setup and procedure
10.7.3.1 Command rate scale factor
10.7.3.1.1 High input rate test
10.7.3.1.2 Low input rate test
10.7.3.1.3 Nonlinearity
10.7.3.1.4 Asymmetry
10.7.3.1.5 Repeatability
10.7.3.1.6 Command rate scale factor sensitivities
10.7.3.1.6.1 Temperature
10.7.3.1.6.2 Magnetic
10.7.3.4 Torquer time constant
10.7.4.1.3 Nonlinearity KTN
10.7.4.1.4 Asymmetry KTA
10.7.4.1.5 Repeatability
10.7.4.1.6 Command rate scale factor sensitivities
10.7.4.1.6.1 Temperature
10.7.4.1.6.2 Magnetic
10.7.4.4 Torquer time constant
10.10.3.1 Alignment of the IRA to the projection of
              the IA on the IRA-SRA plane
10.10.3.2 Alignment of the IA to the IRA-SRA plane
10.10.4.1 Alignment of the IRA to the projection of
              the IA on the IRA-SRA plane
10.13.1 Purpose
10.13.2 Test equipment
10.13.3.5 Anisoinertia drift rate coefficient
10.13.3.5.1 Constant rate method
10.13.3.5.2 Oscillatory method
10.13.3.6 Cross-coupling drift rate
10.13.3.7 Torquer current rectification drift rate
10.13.3.7.1 Angular rate sensing mode, method 1
10.13.3.7.2 Angular displacement-sensing mode (rate-
              integrating mode), method 2
10.13.3.8 Rate hysteresis error
10.13.3.9 Output axis error
10.13.4 Test results
10.13.4.5 Anisoinertia drift rate coefficient
10.13.4.5.1 Constant rate method
10.13.4.5.2 Oscillatory method
10.13.4.6 Cross-coupling drift rate
10.13.4.6.1 Spin-output rectification
10.13.4.6.2 Spin-input rectification
10.13.4.7 Torquer current rectification drift rate
10.13.4.7.1 Angular rate sensing mode, method 1
10.13.4.7.2 Angular displacement-sensing mode (rate-
              integrating mode), method 2
10.13.4.8 Rate hysteresis error
10.13.4.9 Output axis rate error
10.14.2 Test equipment
10.14.3 Test setup and procedure
10.14.3.1 Method 1
10.14.3.2 Method 2
10.14.4 Test results
10.14.4.1 Method 1A
10.14.4.2 Method 2A
10.18 Environmental test series
Table
3 Environmental test series

Abstract

Supplement to IEEE 517 Specifies single-degree-of-freedom rate-integrating gyro as strapdown sensor for (inertial navigation system, attitude reference unit,-----) in (aircraft, missile, -----) application. Gives characteristics of external capture electronics to define performance.

General Product Information

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