兵工自动化2025，Vol.44Issue(3)：70-72,3.DOI:10.7690/bgzdh.2025.03.015
滚转弹舵机延迟时间实时解算方法研究
Research on Real Time Calculation Method of Rudder Engine Delay Time of Rolling Missile
李庚 1王鹏 2高晓波 2娄江 2张瑶 2赵洁 3杜凤怀 2胡车2
作者信息
- 1. 西安现代控制技术研究所第一总体部,西安 710065||北京理工大学宇航学院,北京 100081
- 2. 西安现代控制技术研究所第一总体部,西安 710065
- 3. 北京理工大学宇航学院,北京 100081||北方导航控制技术股份有限公司技术中心,北京 100176
- 折叠
摘要
Abstract
In order to provide accurate parameters for rudder delay phase compensation,a real-time calculation method for rudder delay time of rolling missile was proposed.A/D conversion module is added to the hardware of the computer on the missile to realize the acquisition of the rudder feedback signal,the zero-crossing time of the control command and the rudder deflection angle is calculated according to the periodic zero-crossing characteristics of the control command and the rudder deflection angle of the rolling missile,and the delay time of the rudder engine is calculated according to the zero-crossing time difference.The results show that the delay time calculation module is added in the missile computer software,and the delay time calculation accuracy is improved by linear interpolation,moving average filtering and other methods to meet the guidance and control requirements of the spinning missile.关键词
滚转弹/延迟时间/实时解算/制导控制Key words
rolling missile/delay time/real time calculation/guidance and control分类
军事科技引用本文复制引用
李庚,王鹏,高晓波,娄江,张瑶,赵洁,杜凤怀,胡车..滚转弹舵机延迟时间实时解算方法研究[J].兵工自动化,2025,44(3):70-72,3.
