欢迎来到麦多课文档分享! | 帮助中心 海量文档,免费浏览,给你所需,享你所想!
麦多课文档分享
全部分类
  • 标准规范>
  • 教学课件>
  • 考试资料>
  • 办公文档>
  • 学术论文>
  • 行业资料>
  • 易语言源码>
  • ImageVerifierCode 换一换
    首页 麦多课文档分享 > 资源分类 > PDF文档下载
    分享到微信 分享到微博 分享到QQ空间

    IEEE 293-1969 en Test Procedure for Single-Degree-of-Freedom Spring-Restrained Rate Gyros《单自由度抑跳速率陀螺的试验程序》.pdf

    • 资源ID:1248631       资源大小:1.31MB        全文页数:17页
    • 资源格式: PDF        下载积分:10000积分
    快捷下载 游客一键下载
    账号登录下载
    微信登录下载
    二维码
    微信扫一扫登录
    下载资源需要10000积分(如需开发票,请勿充值!)
    邮箱/手机:
    温馨提示:
    如需开发票,请勿充值!快捷下载时,用户名和密码都是您填写的邮箱或者手机号,方便查询和重复下载(系统自动生成)。
    如需开发票,请勿充值!如填写123,账号就是123,密码也是123。
    支付方式: 支付宝扫码支付    微信扫码支付   
    验证码:   换一换

    加入VIP,交流精品资源
     
    账号:
    密码:
    验证码:   换一换
      忘记密码?
        
    友情提示
    2、PDF文件下载后,可能会被浏览器默认打开,此种情况可以点击浏览器菜单,保存网页到桌面,就可以正常下载了。
    3、本站不支持迅雷下载,请使用电脑自带的IE浏览器,或者360浏览器、谷歌浏览器下载即可。
    4、本站资源下载后的文档和图纸-无水印,预览文档经过压缩,下载后原文更清晰。
    5、试题试卷类文档,如果标题没有明确说明有答案则都视为没有答案,请知晓。

    IEEE 293-1969 en Test Procedure for Single-Degree-of-Freedom Spring-Restrained Rate Gyros《单自由度抑跳速率陀螺的试验程序》.pdf

    1、ANSI/IEEE Std 293-1 969 (IEEE Reaffirmed June 19. 1986) Approved November 17, 1986 American National Standards Institute IEEE Test Procedure for Single-Degree-of-Freedom Spring-Restrained Rate Gyros Published by The Institute of Electrical and Electronics Engineers, Inc 345 East 47th Street, New Yor

    2、k, NY 10017, USA ,A/O/(“/s) at (U,/ (b) Amplitude measurement method, Means of measuring the peak amplitude of the input rate, Means of measuring the in-phase component of the gyro output. 4.22.1.3 Test Setup and Procedure 4.22.1.3.1 Test Setup. Mount the gyro on the oscil- lating rate table with th

    3、e gyro IRA aligned parallel to the axis of the table and nominally vertical. Operate the gyro in accordance with the standard test conditions of paragraph 3.1. Connect the gyro pickoff output and the table rate output to the phase measuring device. 4.22.1.3.2 Test Procedure 4.22.1.3.2.1 Natural Freq

    4、uency. Apply a sinusoidal input of f _ O/s peak. Determine the input frequency f, at which the gyro output lags the input rate by 90 f _ degrees. 4.22.1.3.2.2 Damping Ratio. Apply a sinusoidal input rate of f O/s peak at frequencies of fJa, fJb, , f hertz where a, b, etc., are determined by the user

    5、s requirements. Measure the phase relation between the gyro input and output or 4.22.1.4 Test Results 4.22.1.4.1 Natural Frequency. The natural frequency f. measured in paragraph 4.22.1.3.2.1 shall conform to the requirement of paragraph -. 4.22.1.4.2 Damping Ratio. The damping ratio is cal- culated

    6、 from the data obtained in paragraph 4.22.1.3.2.2 -. by comparing the measured phase relationships with a phase angle-frequency plot for a damped second-order / k measure the peak amplitude of the gyro output. system or by comparing the measured amplitude ratios with an amplitude-frequency plot for

    7、a damped second- order system. The damping ratio shall conform to the requirement of paragraph -. 4.22.2 Step Input Method 4.22.2.1 Purpose. The purpose of this test is to deter- mine the natural frequency and the damping ratio of the gyro by measuring its response to a step input. 4.22.2.2 Test Equ

    8、ipment. The following test equipment from paragraph 3.2 is required for this test: Means of applying a step rate input to the gyro, Means of recording the gyro response to a step rate input. 4.22.2.3 Test Setup and Procedure. Mount the gyro on the step rate table with the gyro IRA aligned parallel t

    9、o the axis of the table and nominally vertical. Operate the gyro in accordance with the standard test conditions of paragraph 3.1. Connect the gyro pickoff output and the table motion output to the recorder. Apply a change of rate from _ O/s to .- f - O/s during a period not to exceed _ seconds. Rec

    10、ord the gyro and the table motion outputs. 4.22.2.4 Test Results. The gyro natural frequency and damping ratio are determined by comparing the recorded response with the step response of a damped second-order system. The natural frequency shall con- form to the requirement of paragraph -, and the da

    11、mping ratio shall conform to the requirement of para- graph - 4.23 Warm-up Time Test 4.23.1 Purpose. The purpose of this test is to determine the time interval required for the gyro to reach specified performance from the instant that it is energized under specified operating conditions. 4.23.2 Test

    12、 Equipment. The following test equipment from paragraph 3.2 is required for this test: Oscillating rate table (means of applying a sinusoidal rate to the gyro at a controlled frequency and am- plitude), Means of measuring the in-phase component of the gyro output, Means of measuring the elapsed time

    13、. 4.23.3 Test Setup and Procedure. Mount the gyro on the oscillating rate table with the gyro IRA aligned parallel to the axis of the table and nominally vertical. Operate the gyro in accordance with the standard test conditions of paragraph 3.1 except that the thermal and mechanical starting condit

    14、ions shall be and the energizing sequence shall be -. 13 14 00 NNN 0 COMMENTS SPECIAL TEST MAY BE RUN TO DETERMINE IF MOTOR REMAINS IN SYNC. CENTRIFUGE TESTS FOR ACCEL-SEWS. DRIFT USUALLY RUN WITH SPIN MOTOR-OFF. SPECIAL TEST MAY SE RUN TO OETERMlNE IF MOTOR REMAINS IN SYNC. SPECIAL TEST MAY BE RUN

    15、TO DETERMINE IF MOTOR REMAINS IN SYNC. PARAMETRIC TESTS TO BE PERFOMEC AT INTERVALS TO BE SPECIFIED FOR EACH TEST. SPECl4L TEST MAY BE RUN TO DETERMINE IF MOTOR REMAINS IN SYNC. SPECIAL TESTS MAY BE ?UN TO DETERMINE IF MOTOR REMAINS IN SYNC. AN0 USING TORQUER TO DETERMINE RATE TRANSFER CHARACTCRISTI

    16、CS. THE HAZARDS OF POST-EXPOSURE HANDLING SHOULD BE CONSIDERED. 15 Apply a sinusoidal input rate of f L_ O/s peak at a frequency of f hertz. Energize the gyro and simultaneously start the elapsed time re- corder. Measure the peak amplitude of the gyro output. When this output reaches - f O/s, stop t

    17、he elapsed time recorder. 4.23.4 Test Results. The elapsed time measured shall conform to the requirement of paragraph -. 4.24 Environmental Test Series Procedures for most environmental tests are well covered by existing industry, government, and military documents, an example of which is MIL-E-527

    18、2, “En- vironmental Testing, Acroiisutical and Associated Equip- ment,” Rather than duplicate samples of existing procedures, this Test Procedure provides assistance in selecting the gyro parameters that will be most im- portant to measure in each environment. This selection is made based on the exp

    19、ected environmental sensitiv- ities of the spring-restrained single-degree-of-freedom rate gyro and the cost effectiveness of the testing. The application of the gyro will determine which tests, or combinations of tests, arc pertinent. 4.24.1 Purpose. The purpose of these tests is to verify that the

    20、 gyro performs as specified during and/or after subjection to environments outside of the standard operating conditions, but within the specified environ- mental limits. 4.24.2 Test Equipment. The following test equipment from paragraph 3.2 is required for each environmental test: Equipment for prov

    21、iding the specified environment, Means of measurement of the environment and time, Adaptation of the gyro to the environmental equipment such as special holding fixtures, cables, etc, Equipment for thc gyro test, chosen as indicated in paragraphs 4.1 through 4.22. 4.24.3 Test Procedure. Detail the p

    22、rocedure for the manipulation of the environment, including the toleranccs and the rates of change, integrated with the procedure for the gyro test. Caution notes on overlosd limits on the environmental intensity applied to the gyro can be specified if required. 4.24.4 Test Results. Parametric test

    23、data shall include the additional notation of the environment in which it was obtained. Where required, the gyro data shall be plotted versus the environmental intensity in order to determine the sensitivity. Table 1 is intended to be a guide for the selection of the gyro test that should be conduct

    24、led in association with the environmental tests that are chosen dependent on the applicatiatl of the gyro. The coding is as follows: D = The gyro parametric test isR-to be conducted while the gyro is operating or nonoperating as applicable, during the specified environment. 0 = The gyro is to be ope

    25、rated during the specified environment and the parametric test performed before and after. N = The gyro is to be nonoperating during the specified environment, and the parametric test performed before and after. S = A special test is recommexletl as described under Comments. When Monitor Output is the requirement, further clari- fication is necessary as to how output variation is to be judged. 16


    注意事项

    本文(IEEE 293-1969 en Test Procedure for Single-Degree-of-Freedom Spring-Restrained Rate Gyros《单自由度抑跳速率陀螺的试验程序》.pdf)为本站会员(appealoxygen216)主动上传,麦多课文档分享仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文档分享(点击联系客服),我们立即给予删除!




    关于我们 - 网站声明 - 网站地图 - 资源地图 - 友情链接 - 网站客服 - 联系我们

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1 

    收起
    展开