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三维目标直接分配新算法
  • ISSN号：1672-7207
  • 期刊名称：中南大学学报(自然科学版)
  • 时间：2013.7.7
  • 页码：385-390
  • 分类：TJ765[兵器科学与技术—武器系统与运用工程]
  • 作者机构：[1]北京航空航天大学飞行器控制一体化技术重点实验室,北京100191
  • 相关基金：航空科学基金资助项目(20080151004);国家自然基金重大研究计划资助项目(90916003,91116002)
  • 相关项目：近空间高超声速飞行器自主协调控制研究
作者： 邵兴悦|任章|廉成斌|
关键词： 切换系统, 滑模, 制导律, 切换律, 保性能控制, switching systems, sliding mode, guidance law, switching functions, guaranteed cost control
中文摘要：

探讨了气动舵面和侧向喷流复合控制模式下拦截弹飞行系统的制导与控制。由于高空气动力不足，同传统的只装配气动舵面的拦截弹相比，为改进对于机动目标的拦截精度，将侧向喷流装置引入以增加导弹的机动能力。使用脉冲型混杂切换系统对侧向喷流导弹动力学进行描述；滑模制导律和决定侧向喷流装置开启策略的逻辑切换律被提出用于产生期望制导指令；仿真和比较证实：滑模制导律和逻辑切换律对目标机动敏感，末端脱靶量很小（〈0.1m），拦截弹动能碰撞杀伤目标。

英文摘要：

Guidance and control law design for an interceptor equipped with both aero fins and side jets was discussed.Since the aerodynamic lift force for generating available norm load is not enough at high altitude,side jets are introduced into the interceptor dynamics to increase its maneuver capability for improving the interception precision to a maneuvering target by comparison with a traditional missile equipped with only aero fins.The side-jet missile dynamics was described with a hybrid impulsive switching system model.A sliding mode guidance law and a logic-based switching function for turning on the side jets were both proposed to generate desired guidance commands.Simulations and comparisons verify that the sliding mode guidance law and logic-based switching law are sensitive to target＇s maneuvering and the end-game miss distance is smaller than 0.1m which represents the interceptor directly hits and kills the target.

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近空间高超声速飞行器自主协调控制研究
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近空间高超声速飞行器飞行姿态/气动力耦合机理与协调控制研究
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期刊信息
  • 《中南大学学报：自然科学版》
  • 北大核心期刊（2011版）
  • 主管单位:教育部
  • 主办单位:中南大学
  • 主编：黄伯云
  • 地址：湖南长沙中南大学校本部
  • 邮编：410083
  • 邮箱：zngdxb@csu.edu.cn
  • 电话：0731-88879765
  • 国际标准刊号：ISSN：1672-7207
  • 国内统一刊号：ISSN：43-1426/N
  • 邮发代号:42-19
  • 获奖情况:
  • 首届全国优秀科技期刊评比一等奖,第二届全国优秀科技期刊评比一等奖,首届中国有色金属工业优秀科技期刊评比一等奖
  • 国内外数据库收录:
  • 美国化学文摘（网络版）,荷兰文摘与引文数据库,美国工程索引,英国科学文摘数据库,中国中国科技核心期刊,中国北大核心期刊（2008版）,中国北大核心期刊（2011版）,中国北大核心期刊（2014版）
  • 被引量:20874