1.
Muzzle Attachment's Influence on the Flying Bullets Attitude of Double-autogun
膛口装置对双联自动机弹丸飞行姿态影响研究
2.
Getting the Attitude of a Rolling Airframe Missile Based on Magneto-resistive Sensor
基于磁阻传感器的旋转弹飞行姿态测量方法
3.
Test and Analysis of Attitude and Movement of Projectile in Bore
弹丸膛内姿态与纵向运动测试与分析
4.
Design and Application of the Bullet Attitude Measurement Record System in Flying Test;
飞行试验用子弹姿态测试记录系统的设计与应用
5.
Multiple Measurement of Trajectory Flying Attitude Angles on the Basis of the Data Fusion of Multisensor and Error Analyse
多传感器数据融合组合测量弹箭飞行姿态及误差分析
6.
THE DESIGN OF THE LARGE CALIBRE GUN MEASURING SYSTEM FOR THE MOTION STATUS OF THE PROJECTILE IN BORE
大口径火炮弹丸膛内运动姿态测试系统设计
7.
Design of Angular Motion Measurement System for Projectiles Based on Fluxgate Sensors
基于磁通门传感器的弹丸姿态角测量系统设计
8.
The design of control system on attitude stability of maneuver re-entry missile head is studied.
对大机动弹头再入飞行段姿态稳定控制系统的设计问题进行了分析与研究。
9.
Study on Attitude Measurement of Gun-Launched Cruise Projectile with Geomagnetic Field
基于地磁场的炮射巡飞弹姿态测量方法研究
10.
An Adaptive Attitude Control Law for Air-launched Cruise Missile
空射飞航导弹姿态控制的一种自适应方法
11.
The Saturn guidance and control systems are designed to provide the proper trajectory and attitude orientation for the vehicle over a range of expected missions.
土星的导引和控制系统的设计能使飞行器在规定的任务范围内提供合适的弹道和姿态方位。
12.
LARGE ANGLE ATTITUDE MANEUVERS AND CONTROLS OF GYROSTAT SPACECRAFT
陀螺体飞行器大角度姿态机动与控制
13.
Research on Attitude Control about Aerospace Vehicle Based on Multi-Agent;
基于多Agent的空天飞行器的姿态控制
14.
Relative Attitude Dynamics and Control in Satellite Formation Flying
卫星编队飞行相对姿态动力学与控制
15.
Adaptive Attitude Coordination Control of Formation Flying Satellite
编队飞行卫星的自适应姿态协同控制
16.
An Aircraft Attitude Indication System Based on MEMS
基于MEMS传感器的飞行姿态指示系统
17.
The stabilization storage of projectile is the precondition of its stabilization flight.
稳定储备量是保证弹丸稳定飞行的前提.
18.
Initial Stage Echo Modeling of Flying Spin-Stabilized Projectile with Slots on Base
底部刻槽旋转稳定弹丸的飞行初始段回波建模