By a known longitudinal scatter of terminal point of self-control phase of a missile, how to find out its intervals of initial altitude that is necessary to definite tactical and technical index, launch mode, combat use, is an inevitable problem to weapon system of a missile based on moving launch plate.
在给定导弹自控终点纵向散布的情况下,如何界定导弹的发射初始姿态域?是动基座发射的导弹武器系统必须面对的问题,它对确定导弹武器系统战术技术指标、发射方式和战斗使用等至关重要。
Designing and Simulating Control System for a Self-rotary Missile of the Air Defense Missile/Gun Weapon System;
弹炮一体化旋转导弹控制系统设计与仿真研究
12,300 Porteous piloted missiles,,,
12300枚先导控制导弹。
The missile is guided by remoter control.
导弹受遥控装置的控制。
antitank missile IR control
反坦克导弹红外控制
Long-distance SINS/GPS Guidance Rocket Projectile Path Control and Simulation;
远程SINS/GPS制导火箭弹弹道控制与仿真
Design of flight training bomb's connected control cabin of guided bomb
制导炸弹飞行训练弹交联控制舱设计
ballistic, guided, nuclear, etc missiles
弹道、 制导、 核...导弹
Design and Research on Simple Guided-bomb's Controllable Ballistic Trajectory;
简易制导炸弹有控弹道的设计与研究
Research of Dynamic and Control of Spinning Ballistic Missile;
弹道导弹滚动飞行动力学与控制研究
Verification and Validation of Controlled Trajectory for Guided Air Ammunition
制导航空弹药有控弹道的校核和验证
Research on Adaptive Fuzzy Sliding Mode Control of Ballistic Missile
弹道导弹的自适应模糊滑模控制研究
Study of Guidance and Control Technigue for ATBM In-atmosphere
大气层内拦截战术弹道导弹制导控制技术研究
Design of Guidance and Control of Air-Launched BTT Missile
空射倾斜转弯导弹制导控制系统设计
Studies of Guidance and Combined Control in Terminal Phase When Intercepting Tactical Ballistic Missile;
拦截战术弹道导弹末段导引和复合控制研究
Design of Integrated Guidance-Control(IGC) System for Beam-Riding Guided Missile
驾束制导导弹一体化制导控制系统设计
Design of the Simulation Console for an Air Launched Guided Munition
某型航空制导弹药仿真控制台的设计
Research of Simply Guided Bomb Flight Control System Simulation;
简易制导炸弹飞行控制系统仿真研究
Research on Safety Control Factors of Winging Missile Developing Enterprises
飞航导弹研制企业安全控制要素研究