inertial missile 中文意思是什麼
inertial missile
解釋
慣性導彈-
The simulation result shows that the influence of the midcourse guidance based on the inertial navigation on the missile ' s impact point is remarkable
模擬結果表明，純慣導中制導對洲際導彈落點精度影響比較大。 -
Gyroscope is indispensable in the control systems and inertial navigation systems on the carriers, such as the plane, the missile, the ship ect
陀螺儀是飛機、導彈、艦船等運載體及慣性導航系統不可缺少的重要元件。 -
The characters of bank - to - turn control technology determine that the btt missile ' s mathematical model having kinematical coupling, aero dynamical coupling, inertial coupling and control coupling. so the widely used stt missile ' s autopilot, which is designed to be three - channel independent ca n ' t meet the btt missile ' s control need
Btt控制技術的控制特點決定了btt導彈的數學模型存在運動學耦合、氣動耦合、慣性耦合和控制耦合等多種耦合因素，因此目前側滑轉彎（ stt ）導彈廣泛採用的自動駕駛儀三通道獨立設計方法已不能滿足btt導彈控制系統的設計要求。 -
One of its distinct character is inertial control and guide missile, which will calculate its ballistic trajectory when the launching point and target point had been fixed, and control system will ascertain it before the missile is launched
作為慣性制導的彈道導彈，其最顯著的一個特點是，當發射點和被打擊的目標一經確定，它的飛行彈道就可相應地計算出來，並在導彈發射前由導彈控制系統予以確定。 -
The ballistic determination, using the orientation information of the sun, the earth, and the moon, is based on an obvious fact, that is, once the “ moon - missile - earth ” angle and the “ sun - missile - earth ” angle observations are only acquired, also with the known inertial positions of the sun and the moon relative to the earth, the inertial position of the missile will be determined uniquely
彈道導彈利用日、地、月方位信息確定位置信息是基於一個明顯的事實:當「月-彈-地」夾角和「日-彈-地」夾角確定時，再加上日、月在地球慣性坐標系下的已知方位，那麼導彈的幾何位置就唯一確定了。 -
Flight test analysis of an improved transfer alignment for missile strapdown inertial guidance system
彈載捷聯慣性制導系統傳遞對準技術試飛驗證 -
Also, the attitude algorithm of the strapdown inertial system of shipboard missile is investigated. on the basis of analysis the sins error model, computer simulation of the sins error are given in accordance with the stochastic error of the inertial instruments
此外，還對艦船捷聯姿態演算法進行了研究，並在分析捷聯系統誤差模型的基礎上，針對慣性元件的隨機誤差給出了捷聯系統的誤差模擬。
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