taptap点点手机网页 ›› 2020, Vol. 38 ›› taptap点点手机网页版 : 27-30.

• 民用航空 • 上一篇    下一篇

六自由度飞行姿态仿真平台设计#br#

杜航航
  

  1. taptap下载安装安卓工程技术训练中心,天津300300
  • 收稿日期:2020-04-21 修回日期:2020-06-17 出版日期:2020-08-27 发布日期:2020-08-27
  • 作者简介:杜航航(1990—),男,河南漯河人,助理工程师,硕士,研究方向为航空电子及民航虚拟仿真技术开发.
  • 基金资助:
    中央高校基本科研业务费专项(3122018S001)

Design of six-DOF attitude simulation system for flight simulator#br#

DU Hanghang#br#   

  1. Engineering Techniques Training Center, CAUC, Tianjin 300300, China
  • Received:2020-04-21 Revised:2020-06-17 Online:2020-08-27 Published:2020-08-27

摘要: 利用Stewart 六自由度并联机构运动学反解控制算法,设计了六自由度飞行姿态仿真平台,将飞行姿态数据转化为执行机构舵机的运动控制参数。通过共享内存方法获取Prepar 3D 模拟飞行软件飞行姿态数据,进而导入仿真平台进行验证,结果表明,该姿态仿真平台运动精度与稳定性较好,适用于理论验证。

关键词: 并联机构, 运动学反解, 舵机, 姿态仿真

Abstract: A six-DOF platform is designed employing the control algorithm of Stewart爷s six-DOF parallel mechanism.Flight attitude data is converted into the actuator motion parameters through inverse kinematics to drive servos.The flight attitude data of Prepar 3D the simulation flight software can be obtained through shared memory and then imported into the simulation platform to conduct verification. Results show that the attitude simulation platform has high motion precision and stability and can be used for theoretical verification.

Key words: parallel mechanism, inverse kinematics, servo, attitude simulation

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