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Therefore the guidance with a limited frame angle range of the image guided aircraft should be studied. The frame angle increases with the decrease of the line-of-sight distance in the three-point guidance, but it is the other way round using the proportional guidance. Therefore, the maximum frame angle is reached when changing the guidance law from the three-point guidance to the proportional guidance. In this paper, a modified proportional navigation is put forward to decrease the frame angle when following a curve escaping target. 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runingTitle=null, highlight=null, articleAbstract=光纤图像制导导弹导引头采取小型化结构,为避免导引过程中发生碰框,需要对导引头框架角进行约束。研究了图像制导导弹在三点法和比例导引法下的需用框架角。结果表明,三点法导引随弹目距离接近需用框架角增大,比例导引法使框架角收敛,由此提出极限框架角时刻,即三点法导引转入比例导引的瞬间。讨论了目标机动对框架角的需求,目标曲线逃逸情况下,单纯的比例导引可能导致追踪过程中导弹框架角发散,由此设计了带有框架角约束的比例导引律。仿真结果表明,加入框架角约束项,能够较为有效地将框架角限制在一个相对较小的波动范围,实现框架角的约束,适用于追踪曲线运动目标。, authors=林德福, 姚怀瑾, 陈方正, authorsList=林德福, 姚怀瑾, 陈方正, authorCompany=北京理工大学宇航学院, 北京 100081, correspAuthors=null, authorNote=林德福,教授,研究方向为飞行器总体,电子信箱:lindf@bit.edu.cn;姚怀瑾,硕士研究生,研究方向为飞行器制导与控制技术,电子信箱:jin_remember@163.com, correspAuthorsNote=null, copyrightStatement=null, copyrightOwner=null, extLink=null, articleAbsUrl=null, sourceXml=null, magXml=null, pdfUrl=null, pdf=8kKNNGn9hF5vbsz5/VTdHQ==, pdfFileSize=3372871, 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)}, authors=null, 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科技导报
| 研究论文 2015, 33(7): 55-60
光纤图像制导导弹导引头框架角分析
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林德福, 姚怀瑾, 陈方正
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Frame angle design of image guided aircraft
Affiliations
出版时间: 2015-04-13
doi: 10.3981/j.issn.1000-7857.2015.07.009
文章导航
光纤图像制导导弹导引头采取小型化结构,为避免导引过程中发生碰框,需要对导引头框架角进行约束。研究了图像制导导弹在三点法和比例导引法下的需用框架角。结果表明,三点法导引随弹目距离接近需用框架角增大,比例导引法使框架角收敛,由此提出极限框架角时刻,即三点法导引转入比例导引的瞬间。讨论了目标机动对框架角的需求,目标曲线逃逸情况下,单纯的比例导引可能导致追踪过程中导弹框架角发散,由此设计了带有框架角约束的比例导引律。仿真结果表明,加入框架角约束项,能够较为有效地将框架角限制在一个相对较小的波动范围,实现框架角的约束,适用于追踪曲线运动目标。
In the design of the image guided bomb, the frame angle varies in a limited range in order to avoid hitting the frame of the miniaturization seeker. Therefore the guidance with a limited frame angle range of the image guided aircraft should be studied. The frame angle increases with the decrease of the line-of-sight distance in the three-point guidance, but it is the other way round using the proportional guidance. Therefore, the maximum frame angle is reached when changing the guidance law from the three-point guidance to the proportional guidance. In this paper, a modified proportional navigation is put forward to decrease the frame angle when following a curve escaping target. The frame angle can thus be limited in a small range according to the simulation results.
frame angle
/
target maneuver
/
guidance law
林德福, 姚怀瑾, 陈方正.
光纤图像制导导弹导引头框架角分析.
科技导报,
2015
, 33
(7)
: 55
-60
.
DOI: 10.3981/j.issn.1000-7857.2015.07.009
LIN Defu, YAO Huaijin, CHEN Fangzheng.
Frame angle design of image guided aircraft[J].
Science & Technology Review ,
2015
, 33
(7)
: 55
-60
.
DOI: 10.3981/j.issn.1000-7857.2015.07.009
2015年第33卷第7期
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doi: 10.3981/j.issn.1000-7857.2015.07.009
接收时间:2014-08-23
首发时间:2015-05-04
出版时间:2015-04-13
收稿日期:2014-08-23
修回日期:2014-11-28
https://castjournals.cast.org.cn/joweb/kjdb/CN/10.3981/j.issn.1000-7857.2015.07.009
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2种不同金属材料的力学参数
科 Family 属数 Number of genus 种数 Number of species 占总种数比例 Percentage of total species (%) 属 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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