首页 | 本学科首页   官方微博 | 高级检索  
     

某型飞机拦阻系统纠偏仿真分析
引用本文:吴娟,何长安. 某型飞机拦阻系统纠偏仿真分析[J]. 系统仿真学报, 2002, 14(12): 1614-1616
作者姓名:吴娟  何长安
作者单位:西北工业大学自动控制系,西安,710072
摘    要:文章建立了某型飞机拦阻系统基于SIMULINK下的飞机撞偏拦阻仿真模型(也适用于非撞偏状况),进行了飞机撞偏阻过程仿真,仿真结果表明,此型飞机拦阻系统对撞偏飞机具有很好的纠偏能力,另外,所建立的仿真模型不仅适用于此型飞机拦阻系统,而且在对模型子系统进行更换后,该撞拦阻仿真模型也适用于其它飞机拦阻系统。

关 键 词:飞机拦阻系统 纠偏 仿真分析 仿真模型
文章编号:1004-731X(2002)12-1614-03
修稿时间:2001-11-27

Simulation Analysis of an Aircraft Arresting System to Rectify a Deviation
WU Juan,HE Chang-an. Simulation Analysis of an Aircraft Arresting System to Rectify a Deviation[J]. Journal of System Simulation, 2002, 14(12): 1614-1616
Authors:WU Juan  HE Chang-an
Abstract:An arresting simulation model of an aircraft arresting system for a certain kind of aircraft which has a deflective engagement of a net barrier is established in this paper (the model is also suitable for normal case). It is based on SIMULINK software. According to the model, arresting process is simulated. Simulation results show that the arresting system is very effective to rectify a deviation of an aircraft having a deflective engagement of a net barrier. The simulation model is not only suitable for the aircraft arresting system, but also suitable for other kinds of aircraft arresting systems by changing the subsystems of it.
Keywords:aircraft arresting system  deviation rectification  simulation analysis  simulation model
本文献已被 CNKI 维普 万方数据 等数据库收录!
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