1. A missile guidance system comprising, a missile carrying a microwave receiver and beam antenna, means adapted to fire said missile in the general direction of a target, a stationary microwave transmitter irradiating said target and its vicinity by a single beam, means conically rotating said ...
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 ...
FIELD: armament, in particular, rocketry, applicable in development of missile systems, for example, with carriers on the ground, in which beam riding guidance systems are used.;SUBSTANCE: electromagnetic radiation from the control point is transformed to electric signals of the missile co-ordinates...
bbs.ccit.edu.cn|基于12个网页 2. 导弹制导系统 导弹制导系统(missile guidance and control system)导引和控 制导弹按选定的规律调整飞行路线并导向目标的全部装置。亦… wenwen.soso.com|基于4个网页 例句
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 and guidance system for guiding a missile The present invention relates to a method and an arrangement for guiding a missile. In accordance with the prior art, the angle position of a target () when the missile () is expected to reach the target is predicted on the basis of the ...
In the sustainer phase of flight, the missile is controlled by an automatic meteorological compensation inertial guidance system (AUTOMET) which controls thrust magnitude. Sustainer control means is provided for varying the thrust of the ... JR MCCORKLE - US 被引量: 25发表: 1971年 AUTOMATIC MIS...
Tactical Missile Guidance and Control System Design(战术导弹制导控制系统设计) 作者:林德福 著出版社:北京理工大学出版社出版时间:2021年03月 手机专享价 ¥ 当当价 降价通知 ¥40.40 定价 ¥62.00 配送至 北京市东城区 运费6元,满49元包邮 服务 由“当当”发货,并提供售后服务。 加入购物车 ...
1. Guided missile having a warhead with a shaped charge which expels energy in a forward direction, a guidance system including a gyroscope located forward of the shaped charge, and the gyroscope having a rotor which has an axis extending from a front end to an aft end of the rotor, a ...