首页> 外文会议>AIAA/ASCE/AHS/ASC structures, structural dynamics and materials conference;AIAA SciTech Forum >Controller Design and Validation of Dynamic Response for Full-Scale Helicopter Flight Simulator at CCSU
【24h】

Controller Design and Validation of Dynamic Response for Full-Scale Helicopter Flight Simulator at CCSU

机译:CCSU大型直升机飞行模拟器动态响应控制器设计与验证

获取原文

摘要

A research team comprised of students and faculty from Central Connecticut State University's (CCSU) School of Engineering, Science, and Technology has begun the design, production, and testing of a full-scale helicopter flight simulator with a moving platform. This paper will present the system identification, controller tuning and validation, and comparison of simulator dynamics against available helicopter dynamic models during typical flight maneuvers. The purposes for conducting this research include: i) to build a fully functional flight simulator that can be used as a test bed for students research projects; ii) to apply theoretical lessons of control of dynamic systems to a real, tangible electromechanical system; iii) to provide students with hands-on experience on how to design and fly a helicopter. CCSU students have built and programed all of the mechanical and electrical systems. The basic design weight for the simulator is 300 lbs force applied to the pilot seat. The structures are designed to have enough strength to sustain a maximum of 3g and a minimum -lg flight conditions. There are three actuators in place that can be used to rotate the platform in the pitching, rolling, and yawing directions. All electrical systems were designed, fabricated, and assembled by CCSU students. The controller was designed and implemented by the students and faculty of CCSU.
机译:由中央康涅狄格州立大学(CCSU)工程,科学和技术学院的师生组成的研究团队已开始设计,生产和测试带有移动平台的全尺寸直升机飞行模拟器。本文将介绍系统识别,控制器调整和验证,以及在典型的飞行演习中将模拟器动力学与可用直升机动力学模型进行比较。进行这项研究的目的包括:i)建立一个功能齐全的飞行模拟器,可以用作学生研究项目的试验台; ii)将动态系统控制的理论课程应用于实际的有形机电系统; iii)为学生提供有关如何设计和驾驶直升机的动手经验。 CCSU的学生已经构建并编程了所有机械和电气系统。模拟器的基本设计重量是施加在飞行员座椅上的300磅力。这些结构的设计强度足以承受最大3g的飞行力和最小-lg的飞行条件。共有三个执行器,可用于在俯仰,滚动和偏航方向上旋转平台。所有电气系统都是由CCSU学生设计,制造和组装的。该控制器由CCSU的学生和教职员工设计和实施。

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