首页 | 本学科首页   官方微博 | 高级检索  
     

关于柔性航天器动力学模型降阶问题
引用本文:缪炳祺,曲广吉,夏邃勤,程道生. 关于柔性航天器动力学模型降阶问题[J]. 中国工程科学, 2001, 3(11): 70-73
作者姓名:缪炳祺  曲广吉  夏邃勤  程道生
作者单位:1. 浙江工业大学机电学院,杭州,310014
2. 北京空间飞行器总体设计部,北京,100086
摘    要:针对柔性航天器动力学模型的降阶问题,综述了动力学建模中几种常用的模态集,介绍了用于选择系统保留模态的有关准则。通常的模态价值分析和内平衡理论是用于航天器系统模态的选取,而不是直接用于动力学建模时的部件模态或系统结构弹性变形模态的选取,因而存在如何应用上述准则于动力学建模的问题。为此,提出了一个动力学建模时的降阶策略;还提供了一个数值例子,以对采用不同的模态集建模时的结果进行比较,并表明如何采用上述准则于航天器的动力学建模。

关 键 词:航天器;柔性体;动力学;模型降阶
收稿时间:2001-04-16
修稿时间:2001-04-25

Experiments on a Secondary Regulated Loading System
miubingqi,quguangji,xialiule and chengdaosheng. Experiments on a Secondary Regulated Loading System[J]. Engineering Science, 2001, 3(11): 70-73
Authors:miubingqi  quguangji  xialiule  chengdaosheng
Abstract:With secondary regulation, a novel hydraulic transmission technology,the secondary regulated loading system described here is oriented to rotational speed experiment of reduction gear or material. In this paper, the hardware structure of the system is introduced with specialties of the transducers, electro|hydraulic servo valves and the computer data collector used. Then, signal|adjusting circuit between computer control system and transducers or servo valves is designed. Next, a VC++ control program under Windows operating system is worked out. Experiments on Step, Rectangle, Ramp and Sine Responses of the speed sub|system are done under alternative oil pressure and load. Finally, some meaningful results are given by contrasting the experimental curves. [
Keywords:hydrostatic driving  secondary regulation  loading  experiments
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《中国工程科学》浏览原始摘要信息
点击此处可从《中国工程科学》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号