首页> 外文期刊>日本航空宇宙学会論文集 >Flight Simulator Experiments on the Effects of Control System Dynamics to Airplane's Flying Qualities
【24h】

Flight Simulator Experiments on the Effects of Control System Dynamics to Airplane's Flying Qualities

机译:控制系统动力学对飞机飞行质量影响的飞行模拟器实验

获取原文
获取原文并翻译 | 示例
           

摘要

Fixed base flight simulator experiments were conducted to investigate effects of control system dynamics on the handling qualities of an airplane. Breakout forces and force gradient ratio to control displacement were changed mechanically by the ELECTRO-LOAD equipped to the simulator recently. Relationships between control forces and stick positions were measured, and both breakout forces and force gradient ratio were determined experimentally.
机译:进行了固定基础飞行模拟器实验,以研究控制系统动力学对飞机操纵质量的影响。最近通过安装在模拟器上的ELECTRO-LOAD机械地改变了用于控制位移的爆发力和力梯度比。测量了控制力和操纵杆位置之间的关系,并通过实验确定了爆发力和力梯度比。

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