• 主题
高级搜索  >
历史搜索 清空历史
首页> 美国政府科技报告 >Feasibility Study on the Implementation of a Given Hydraulic Servo Actuator inthe Cessna Citation II Elevator Flight Control System
【24h】

Feasibility Study on the Implementation of a Given Hydraulic Servo Actuator inthe Cessna Citation II Elevator Flight Control System

机译：Cessna Citation II电梯飞行控制系统中给定液压伺服作动器实施的可行性研究

获取原文
页面导航
  • 摘要
  • 著录项
  • 相似文献
  • 相关主题

摘要

This report contains the results of a feasibility study on the implementation ofa given hydraulic servoactuator in parallel with conventional elevator flight control system (EFCS) of the Cessna Citation II. For this purpose, a nonlinear elevator model and servoactuator model is derived. Firsty, the performance diagram for sinusoidally movement of the elevator control surface with a simplified elevator model is presented. Thereafter, dynamic analysis of the two integrated models follows. An autopilot is designed to verify the servoactuator controller design for representative control tasks and responses on turbulence. For the aircraft model, the similar Cessna Citation 500 was used. Simulations were done with the use of the software package DASMAT.

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