IEEE-517-1973-R2005.pdf
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1、Recognized as an American National Standard (ANSI) Copyright 1974 by The Institute of Electrical and Electronics Engineers, Inc. SECOND PRINTING: 15 February 2008. Errata can be found at: http:/standards.ieee.org/reading/ieee/updates/ errata/index.html. No part of this publication may be reproduced
2、in any form, in an electronic retrieval system or otherwise, without the prior written permission of the publisher. IEEE Std 517-1974(R2005) IEEE Standard Specification Format Guide and Test Procedure for Single-Degree-of-Freedom Rate- Integrating Gyros Sponsor Gyro and Accelerometer Panel of the IE
3、EE Aerospace Electronics System Society Reaffirmed November 8, 2005 Approved December 13, 1973 IEEE Standards Board Reaffirmed June 7, 2000 Approved May 30, 1983 American National Standards Institute Copyright The Institute of Electrical and Electronics Engineers, Inc. Provided by IHS under license
4、with IEEELicensee=IHS Employees/1111111001, User=Japan, IHS Not for Resale, 07/30/2008 02:23:47 MDTNo reproduction or networking permitted without license from IHS -,-,- ii Approved December 13, 1973 IEEE Standards Board Robert D. Briskman , Chair Sava I. Sherr , Secretary Stephen J. Angello Saul Ar
5、onow James E. Beehler Richard Brereton Warren H. Cook Louis Costrell Jay Forster Joseph L. Koepfinger William R. Kruesi Benjamin J. Leon Donald T. Michael Voss A. Moore James D. M. Phelps Saul W. Rosenthal Gustave Shapiro Ralph M. Showers Robert A. Soderman Frederick G. Timmel Leendert van Rooij Rob
6、ert V. Wachter Bruno O. Weinschel William T. Wintringham Copyright The Institute of Electrical and Electronics Engineers, Inc. Provided by IHS under license with IEEELicensee=IHS Employees/1111111001, User=Japan, IHS Not for Resale, 07/30/2008 02:23:47 MDTNo reproduction or networking permitted with
7、out license from IHS -,-,- iii Foreword (This foreword is not a part of IEEE Std 517-1974, Specifi cation Format Guide and Test Procedure for Single-Degree-of-Freedom Rate-Integrating Gyros.) This standard was prepared by the Gyro and Accelerometer Panel of the Aerospace Electronics Systems Society
8、of the Institute of Electrical and Electronics Engineers. It consists of two parts. Part I is a specifi cation format guide for the preparation of a rate-integrating gyro specifi cation. It provides a common meeting ground of terminology and practice for manufacturers and users. The user is cautione
9、d not to overspecify; only those parameters that are required to guarantee proper instrument performance in the specifi c application should be controlled. In general, the specifi cation should contain only those requirements that can be verifi ed by test or inspection. Parameters in addition to tho
10、se given in this standard are not precluded. Figs 1 and 2 are to be used as a guide for the preparation of specifi c fi gures or drawings. Part II is a compilation of recommended procedures for testing a rate-integrating gyro. These procedures, including test conditions to be considered, are derived
11、 from those currently in use. For a specifi c application, the test procedure should refl ect the requirements of the specifi cations; therefore, not all tests outlined in this document need be included, nor are additional tests precluded. In some cases, alternative methods for measuring performance
12、 characteristics have been included or indicated. The intent is for the specifi cation writer to extract the applicable test conditions and equipment requirements from Section 9. for inclusion in the appropriate sections listed under Section 4.5. Similarly, it is intended that the writer extract the
13、 applicable test procedures from Section 10. for inclusion in the appropriate sections listed under Section 4.6. Part II can also be used as a guide in the preparation of a separate rate-integrating gyro test specifi cation with appropriate section numbering. Blank spaces in the text of this documen
14、t permit the insertion of specifi c parameter values and their tolerances. Brackets are used to enclose alternative choices of dimensional units, signs, axes, etc. Boxed statements are included for information only and are not part of the specifi cation or test procedures. The symbols used conform t
15、o IEEE Std 260-1967 , Letter Symbols for Units Used in Electrical Science and Electrical Engineering. Terminology used conforms to Aerospace Industries Association EETC Report 5 (Revision A), Standard Gyro Terminology. This document defi nes the requirements and test procedures for a conventional si
16、ngle-degree-of-freedom rate- integrating gyro in terms of characteristics unique to the gyro. The requirements contained herein are intended to cover applications in which the dynamic angular inputs to which the gyro is subjected are benign relative to the accuracy required. This will cover most gim
17、balled platform applications and those nongimballed applications (for example, space vehicle attitude control systems) in which the dynamic inputs are not so severe as to make additional parameters signifi cant. The rate-integrating gyro provides a voltage output proportional to angular displacement
18、 of the case about the input axis when in an open-loop mode or when captured by a servoed platform, or a current proportional to angular rate about the input axis when captured through an external loop using the gyro torquer. A model equation is given in Section 6.3 for reference, to be included in
19、a specifi cation only to the extent necessary. Appendix A lists various rate-integrating gyro design features for which this format is applicable. The table is not intended to make any suggestion regarding the selection of particular design features that might restrict the free choice of manufacture
20、rs. Copyright The Institute of Electrical and Electronics Engineers, Inc. Provided by IHS under license with IEEELicensee=IHS Employees/1111111001, User=Japan, IHS Not for Resale, 07/30/2008 02:23:47 MDTNo reproduction or networking permitted without license from IHS -,-,- iv The IEEE will maintain
21、this document current with the state of the technology. Comments are invited on this document as are suggestions for additional material. These should be addressed to: Secretary IEEE Standards Board The Institute of Electrical and Electronics Engineers, Inc 345 East 47 Street New York, N.Y. 10017 Th
22、is publication represents a group effort on a large scale. A total of 167 individuals attended 37 meetings of the Gyro and Accelerometer Panel while work on this standard was in progress. The following members were responsible for this work: R. B. Clark (Chairman, 1967) C. O. Swanson (Chairman, 1968
23、) H. A. Dinter (Chairman, 1969) N. F. Sinnott (Chairman, 1970) M. D. Mobley (Chairman, 1971) K. W. Homb (Chairman, 1972) A. T. Campbell (Chairman, 1973) A. M. Brady R. M. Burrows R. A. Crawford H. B. Diamond J. DiGirolamo E. G. Fotou H. A. Fredine T. A. Fuhrman K. N. Green H. L. Gubbins J. E. Hardie
24、 J. G. Hawkins C. E. Hurlburt J. V. Johnston C. A. Jones J. H. Jordan K. J. Klarman J. Koestler W. G. Lane A. A. Lee A. M. Leeking F. B. Mikoleit G. E. Morrison G. H. Neugebauer T. M. Rankin R. F. Rathcke H. F. Rickman H. Rogall L. M. Ross R. C. Royce C. W. Spencer C. I. Thornburg R. L. Van Alstine
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