航空学报 > 1990, Vol. 11 Issue (4): 171-176

实时计算机力控制系统的一种设计方法

蔡小斌, 戴冠中   

  1. 西北工业大学
  • 收稿日期:1988-08-06 修回日期:1900-01-01 出版日期:1990-04-25 发布日期:1990-04-25

A DESIGN METHOD FOR REAL-TIME COMPUTER CONTROL HYDRAULIC FORCE SYSTEM

Cai Xiaobin, Dai Guanzhong   

  1. Northwestern Polytechnical University
  • Received:1988-08-06 Revised:1900-01-01 Online:1990-04-25 Published:1990-04-25

摘要: 本文给出用于实时计算机力控制系统的、具有条件输出反馈的数字控制器的设计方法。文中讨论了条件反馈控制器的基本原理、结构以及设计方法。该控制器应用于变后掠机翼的结构强度加载控制系统之中。试验结果表明,本文提出的方法具有跟踪精度高、抗干扰能力强、重复工作性能好的优点。试验结果是优良的。

Abstract: In this paper, a method of designing the digital controller for real-time computer control hydraulic force system with conditional output feedback is presented. ’The basic principle, the construction of conditional feedback controller, and the design procedure are discussed. This controller is applied to the structural strength loading control system, which is the experimental system of a variable swept aircraft wing. Experiments show that the design method presented in this paper is feasible and the results are quite good.