244/3.22 Other Classes: 244/79 International Classes: F02K9/84 View Patent Images: Download PDF 3249325 US Patent References: 2995319A pre-boost control device for aerial missiles1961-08-08 2754789Gyro controlled steering system1956-07-17
PURPOSE: To provide a guidance system for a homing missile including an observation filter using a distance, a distance rate, right-angled acceleration with respect to a line of sight of the missile, acceleration along the line of sight of the missile and the line of sight of the missile ...
PROBLEM TO BE SOLVED: To provide a missile guidance system capable of shooting down a target at a high altitude region without increasing a weight of the missile and without making any large-sized formation of the missile.SOLUTION: A swing motion acceleration limit function {n=f(t)} is a ...
The invention relates to missile guidance and provides a method and system for guiding one or more missiles on to one or more targets. Aim on the targets and missiles is taken by means of two electro-
Missile-guidance system and guided missile 专利名称：Missile-guidance system and guided missile 发明人：Ottenheimer, Philippe,Haon, Pierre 申请号：EP80400837.3 申请日：19800610 公开号：EP0021944A1 公开日：19810107 专利内容由知识产权出版社提供 专利附图：摘要：Array 申请人：THOMSON-CSF 地址：173, ...
PROBLEM TO BE SOLVED: To provide a guidance and control system and a method for making an intercepting missile for intercepting a TBM coming flying outside the atmosphere hit directly the TBM with high precision of about ten-odd cm by the final movement at the final stage in the closing per...
GUIDANCE SYSTEM AND MISSILE GUIDANCE METHO 专利名称：MISSILE GUIDANCE SYSTEM AND MISSILE GUIDANCE METHOD 发明人：SODA MAKOTO,左右田 真 申请号：JP2006052316 申请日：20060228 公开号：JP2007232254A 公开日：20070913 专利内容由知识产权出版社提供 专利附图：摘要：Array 申请人：TOSHIBA CORP,株式会社東芝 ...
A terminal miss sensitivity analysis was performed for a linearized, time invariant missile system in a two dimensional plane. First the missile system equ... kjesbo,lee a 被引量: 0发表: 1974年 Automatic missile guidance system and missile provided with such a system not available for EP022892...
MISSILE AND MISSILE GUIDANCE SYSTEM 专利名称：MISSILE AND MISSILE GUIDANCE SYSTEM 发明人：ASHIHARA TORU,芦原 徹 申请号：JP2006071000 申请日：20060315 公开号：JP2007247952A 公开日：20070927 专利内容由知识产权出版社提供 专利附图：摘要：Array 申请人：MITSUBISHI ELECTRIC CORP,三菱電機株式会社地址：東京都...