首页> 美国政府科技报告 >ANALYSIS AND COMPENSATION OF AN AIRCRAFT SIMULATOR CONTROL LOADING SYSTEM WITH COMPLIANT LINKAGE
【24h】

ANALYSIS AND COMPENSATION OF AN AIRCRAFT SIMULATOR CONTROL LOADING SYSTEM WITH COMPLIANT LINKAGE

机译:具有顺应连接的飞机模拟器控制负载系统的分析与补偿

获取原文

摘要

A hydraulic control loading system for aircraft simulation was analyzed to find the causes of undesirable low frequency oscillations and loading effects in the output. The hypothesis of mechanical compliance in the control linkage was substantiated by comparing the behavior of a mathematical model of the system with previously obtained experimental data.nA compensation scheme based on the minimum integral of the squared difference between desired and actual output was shown to be effective in reducing the undesirable output effects. The structure of the proposed compensation was computed by use of a dynamic programing algorithm and a linear state space model of the fixed elements in the system.

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号