missile attitude的意思

missile attitude中文翻譯：

飛彈姿態

相似詞語短語

missile───adj.導彈的；可投擲的；用以發射導彈的；n.導彈；投射物

attitude───n.態度；看法；意見；姿勢

regulus missile───雷格斯導彈

furnishes attitude───提供態度

fagot missile───法格特導彈

cruise missile───n.巡航導彈；n.[航][軍]巡航導彈

attitude to───vt.對...態度，看法

missile defense───導彈防御

blowgun missile───噴槍導彈

雙語使用場景

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.───研究具有大離軸角及越肩發射能力的先進空空導彈初始段敏捷轉彎方法，研究了裝有反作用噴氣控制系統的空空導彈的大角度姿態過失速機動控制律。

Microwave phase shifter in phased-array radar, communications, instrumentation, heavy ion accelerator and the missile attitude control system has a broad application prospects.───微波移相器在雷達、通信、儀器儀表、重離子加速器及導彈姿態控制系統中有著廣泛的應用前景。

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.───變結構控制作為控制系統的一種綜合方法，它的滑動模態具有不變性，這是變結構控制在導彈姿態控制中最突出的優點。

The Variable Structure Adaptive Control and its Application to Missile Attitude Control System───戰略導彈姿態系統的變結構自適應控制研究

Study on the Change of the Roll Rate and Its Effect on Missile Attitude for Mass Moment Control Missile───兩質量塊質量矩控制導彈滾轉速度的變化及對彈體姿態運動影響分析

Determination of the Optimal Testing Points for Missile Attitude Control System───導彈姿態控制系統最佳測試點的選取

Application of a New Control Law to Missile Attitude Control System───新型變結構控制律在導彈姿態控制系統中的應用

Discrete Variable Structure Control of Missile Attitude Control System───數字式導彈姿態控制系統的變結構控制

Application of Optimal Control Using Direct Side Force in Missile Attitude Control System───最優控制與姿控噴流在導彈姿態控制中的應用

英語使用場景

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.