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For a large motor and sustained high speed targets, the guidance performance will be better with the direct force control., authors=ZHAN Jianchao, GENG Guanglong, MA Xiaoxiao, RONG Penghui, authorsList=ZHAN Jianchao;GENG Guanglong;MA Xiaoxiao;RONG Penghui, authorCompany=Department of Aviation Ammunition, Xuzhou Air Force College, Xuzhou 221000, Jiangsu Province, China, correspAuthors=null, authorNote=null, correspAuthorsNote=null, copyrightStatement=null, copyrightOwner=null, extLink=null, articleAbsUrl=null, sourceXml=null, magXml=null, pdfUrl=null, pdf=j6ojA1W62RXpV5KRVt57ZA==, pdfFileSize=1175746, pdfExtLink=null, richHtmlUrl=null, mobilePdfUrl=null, reviewReport=null, pdfFirstPage=null, abstractGraph=null, abstractGraphContent=null, abstractVideo=null, citation=null, cebUrl=null, magXmlContent=null, mapNumber=null, fund=null), CN=ArticleExt(id=1242129114275054143, articleId=1242129112886739508, tenantId=1146029695717560320, journalId=1146031591421210625, language=CN, 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空空导弹ENDGAME段导引律研究
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科技导报 | 研究论文 2012,30(20): 71-74
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科技导报 | 研究论文 2012, 30(20): 71-74
空空导弹ENDGAME段导引律研究
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展建超, 耿广龙, 马潇潇, 荣鹏辉
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    徐州空军学院航空弹药系,江苏徐州 221000
ENDGAME Guidance Law of Air-to-air Missile
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出版时间: 2012-07-18 doi: 10.3981/j.issn.1000-7857.2012.20.012
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针对空空导弹ENDGAME段,选择合适的导引律,对导弹能否精确打击目标至关重要。本文分析了比例导引律、微分对策导引律和变结构导引律3种不同导引律的设计思路,并引入直接力控制,针对不同攻击条件进行计算机仿真分析。仿真结果表明,在迎击条件下,变结构和微分对策导引律较比例导引律更优,对大机动、持续高速运动的目标,具有直接力控制的制导性能更好。
空空导弹  /  ENDGAME  /  导引律  /  微分对策  /  变结构控制
For the ENDGAME section of air-to-air missiles, it is very important to select an appropriate guidance law for missile to hit targets accurately. This paper analyzes three different guidance laws, that is, the proportional guidance law, the differential game guidance law and the variable structure guidance law. The direct force control is introduced, and then the performance of three different guidance laws under various attack conditions is analyzed by the computer simulation. It is shown that under the engaged condition, the variable structure and the differential game guidance laws are better than the proportional navigation law. For a large motor and sustained high speed targets, the guidance performance will be better with the direct force control.
air-to-air missile  /  ENDGAME  /  guidance law  /  differential game  /  variable structure control
展建超;耿广龙;马潇潇;荣鹏辉. 空空导弹ENDGAME段导引律研究. 科技导报, 2012 , 30 (20) : 71 -74 . DOI: 10.3981/j.issn.1000-7857.2012.20.012
ZHAN Jianchao;GENG Guanglong;MA Xiaoxiao;RONG Penghui. ENDGAME Guidance Law of Air-to-air Missile[J]. Science & Technology Review, 2012 , 30 (20) : 71 -74 . DOI: 10.3981/j.issn.1000-7857.2012.20.012
2012年第30卷第20期
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doi: 10.3981/j.issn.1000-7857.2012.20.012
  • 接收时间:2012-04-17
  • 首发时间:2012-07-18
  • 出版时间:2012-07-18
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  • 收稿日期:2012-04-17
  • 修回日期:2012-07-02
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2种不同金属材料的力学参数

Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)

Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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