missile attitude发音

意思翻译

飞弹姿态

相似词语短语

missile───adj.导弹的；可投掷的；用以发射导弹的；n.导弹；投射物

attitude───n.态度；看法；意见；姿势

regulus missile───雷格斯导弹

furnishes attitude───提供态度

fagot missile───法格特导弹

cruise missile───n.巡航导弹；n.[航][军]巡航导弹

attitude to───vt.对...态度，看法

missile defense───导弹防御

blowgun missile───喷枪导弹

双语使用场景

This paper investigates the large Angle attitude post stall maneuver control for the agile turn phase of an air-to-air missile that has high off-boresight capability and head reverse maneuverability.───研究具有大离轴角及越肩发射能力的先进空空导弹初始段敏捷转弯方法，研究了装有反作用喷气控制系统的空空导弹的大角度姿态过失速机动控制律。

Microwave phase shifter in phased-array radar, communications, instrumentation, heavy ion accelerator and the missile attitude control system has a broad application prospects.───微波移相器在雷达、通信、仪器仪表、重离子加速器及导弹姿态控制系统中有着广泛的应用前景。

As a synthesis method in control system, the sliding mode of variable structure control is invariable, and which is its most excellent advantage in the missile attitude control system.───变结构控制作为控制系统的一种综合方法，它的滑动模态具有不变性，这是变结构控制在导弹姿态控制中最突出的优点。

The Variable Structure Adaptive Control and its Application to Missile Attitude Control System───战略导弹姿态系统的变结构自适应控制研究

Study on the Change of the Roll Rate and Its Effect on Missile Attitude for Mass Moment Control Missile───两质量块质量矩控制导弹滚转速度的变化及对弹体姿态运动影响分析

Determination of the Optimal Testing Points for Missile Attitude Control System───导弹姿态控制系统最佳测试点的选取

Application of a New Control Law to Missile Attitude Control System───新型变结构控制律在导弹姿态控制系统中的应用

Discrete Variable Structure Control of Missile Attitude Control System───数字式导弹姿态控制系统的变结构控制

Application of Optimal Control Using Direct Side Force in Missile Attitude Control System───最优控制与姿控喷流在导弹姿态控制中的应用

英语使用场景

Microwave phase shifter in phased-array radar, communications, instrumentation, heavy ion accelerator and the missile attitude control system has a broad application prospects.

The corrective network is an important component of the missile attitude control system.

Strap-down seeker's detecting information is coupled with missile attitude information, hence it can't be used for proportional navigation directly.

A free gyro is generally used as the reference for missile attitude control in the control system of antitank missiles, and the gyro-rotor in such cases is often spun in inertial rundown.