首页 | 本学科首页   官方微博 | 高级检索  
     检索      

瞬态气动模拟加热控制中的快速高精度"E-T"转换
引用本文:吴大方,贺小帆,高镇同.瞬态气动模拟加热控制中的快速高精度"E-T"转换[J].北京航空航天大学学报,2002,28(1):90-93.
作者姓名:吴大方  贺小帆  高镇同
作者单位:北京航空航天大学 飞行器设计与应用力学系
基金项目:航空科研项目;98I51040;
摘    要:为了准确模拟飞行器在高速飞行时的瞬态气动加热状态,必须使用快速、高精度的计算机瞬态热能控制系统,对气动模拟试验的加热过程,实行快速、高精度的非线性动态控制.为此,传感器的快速、高精度"E-T"转换是一个必须解决的非常重要的问题.提出一种高速飞行器瞬态气动加热控制系统中传感器的快速、高精度"E-T"转换方法.该方法具有计算简单、转换速度快、校正精度高的优点,使用该方法实现了高速飞行器气动加热过程中温度场高速变化状态下的瞬态非线性动态控制.

关 键 词:传感器  动态响应  非线性  气动加热  实时转换
文章编号:1001-5965(2002)01-0090-04
收稿时间:2000-06-05
修稿时间:2000年6月5日

High Speed and Accurate "E-T" Translation Method for Transient Aerodynamic Heating Control System
WU Da,HE Xiao,GAO Zhen.High Speed and Accurate "E-T" Translation Method for Transient Aerodynamic Heating Control System[J].Journal of Beijing University of Aeronautics and Astronautics,2002,28(1):90-93.
Authors:WU Da  HE Xiao  GAO Zhen
Institution:Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics
Abstract:To simulate the transient aerodynamic heating condition of high speed flight vehicle, the high speed and accurate computer transient control system must be used to realize the high speed nonlinear dynamic controlling in the heating process of aerodynamic simulation experiment. To reach this aim, a very important problem of high speed and accurate E T translation of sensor must be solved. A high speed and accurate E T translation method of sensor for transient aerodynamic heating control system of high speed flight vehicle is proposed. This method possesses many advantages, such as, easy to calculation, with high translating speed and high accurate calibration. Using this method, the transient nonlinear dynamic controlling in the aerodynamic heating process of high speed flight vehicle and under high speed variable temperature field has been realized.
Keywords:sensors  dynamic response  non  linear  aerodynamic heating  real  time translation  
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《北京航空航天大学学报》浏览原始摘要信息
点击此处可从《北京航空航天大学学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号