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Conversion of a C-11B instrument flight trainer into a variable stability flight simulator.

机译:将C-11B仪表飞行教练机转换为可变稳定性飞行模拟器。

摘要

A C-11B Instrument Flight Trainer was converted into a variablestability flight simulator. The original frame, cockpit, controls,pneumatic system and instruments were utilized as well as certain othernecessary components. The original aerodynamic and engine computerswere removed, a new instrument drive system was designed and a hybridcomputer was programed to solve the equations of motion. The cockpitcontrols supplied the inputs to the computer which in turn supplied theoutputs to the various instruments through their respective drivesystems. The computer program may be quickly changed to simulate theaerodynamic characteristics of almost any single engine jet aircraft,or the parameters of a specific aircraft may be varied to investigatetheir effects on flying qualities.
机译:一架C-11B仪表飞行教练员被转换为可变稳定性飞行模拟器。使用了原始的车架,驾驶舱,控件,气动系统和仪器以及某些其他必要的组件。拆除了原始的空气动力学和发动机计算机,设计了新的仪表驱动系统,并编写了混合动力计算机来求解运动方程。座舱控制器将输入提供给计算机,计算机又通过各自的驱动系统将输出提供给各种仪器。可以快速更改计算机程序以模拟几乎任何单引擎喷气飞机的空气动力学特性,或者可以更改特定飞机的参数以研究其对飞行质量的影响。

著录项

  • 作者

    Sweeney Charles John Jr;

  • 作者单位
  • 年度 1968
  • 总页数
  • 原文格式 PDF
  • 正文语种 en_US
  • 中图分类

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