PURPOSE:To make it possible to simplify the structure of an automatic trancking system and also to reduce the agitation of a beam due to a scan, by taking the scan with an electric seeker axis agreeing with a missile axis. CONSTITUTION:As for the homing guidance system for a 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 ...
In a CLOS missile guidance system, target and missile tracking data e.g. video image data are acquired on a UAV and transmitted to the missile where they are processed to provide guidance control data to the missile. Alternatively the video image data may be transmitted to a command station ...
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, ...
Method of combined guidance of small-sized missile with separable propulsion system and guidance system for its implementation FIELD: weapon and ammunition. SUBSTANCE: method includes formation of an information field of control, start of the missile at an angle to the line of vising of the target...
FIELD: missile guidance systems, applicable for guidance of missiles launched from sea carriers, for instance, from boats. SUBSTANCE: system has a sight with sensors of angular rate and angular position of the sighting line in two mutually orthogonal planes, guidance unit forming the guidance comman...
Trajectory-Shape-Varying Missile Guidance for Interception of Ballistic Missiles during the Boost Phase 热度: 页数:21 Aegis Missile Guidance System SPY-1D(V) Transmitter and MK 99 Fire 热度: 页数:2 ch07Strategic and Tactical Supply Chain Planning State-of-the-art Modeling Applications 热度...
This paper overviews development of the guidance and control system design of the Multimode Airframe Technology (MAT) missile being developed at the Missil... Justin L. S. Walls 被引量: 1发表: 1998年 THE INTEGRATION OF SPC WITH AUTOMATIC TEST EQUIPMENTS: A CASE STUDY nature of SPC, an aut...
This invention relates generally to missile directional control systems and, more particularly, to a directional control system to provide missile guidance during its high acceleration boost flight. In provision of a directional control system, a primary requirement is that the missile be aligned in th...
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...