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战术飞行实时轨迹优化系统设计
引用本文:胡昱,夏洁,高金源. 战术飞行实时轨迹优化系统设计[J]. 飞行力学, 2001, 19(2): 26-29
作者姓名:胡昱  夏洁  高金源
作者单位:北京航空航天大学自动控制系,
基金项目:航空基金资助项目 ( 98E51 0 0 9)
摘    要:介绍了在所开发的“战术飞行轨迹优化系统”中采用的轨迹优化方法-启发式搜索算法的改进方案。为了加快搜索速度,建立了专家系统,介绍了专家系统的规则。为了验证方法的有效性,建立了基于局域网的地面实时仿真系统,详细介绍了专家系统的设计。仿真计算结果表明,所开发的飞行轨迹优化系统是可行的。

关 键 词:战术飞行 轨迹优化系统 启发式搜索算法 专家系统 设计 地面实时仿真系统
文章编号:1002-0853(2001)02-0026-04
修稿时间:2000-07-05

Design of the tactical flight real-time optimal trajectory system
HU Yu,XIA Jie,GAO Jin yuan. Design of the tactical flight real-time optimal trajectory system[J]. Flight Dynamics, 2001, 19(2): 26-29
Authors:HU Yu  XIA Jie  GAO Jin yuan
Abstract:In this paper, the improve method on heuristic search algorithm is presented that is used in the developed tactical flight optimal trajectory system To make the search speeds fast, an expert system was established The rules on expert system are also presented In order to evaluate an efficient of the method, the real time simulation system on the basis of network is made up The detailed design of the simulation system is given The result of simulation show that the developed simulation system is an efficient
Keywords:tactical flight management system  tactical flight trajectory optimization  artificial intelligent  heuristic search method  expert system
本文献已被 CNKI 维普 万方数据 等数据库收录!
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