attitude jet 中文意思是什麼
attitude jet
解釋
空氣噴氣發動機-
The control method of side jet and aerodynamic compound control, including side jet and aerodynamic compound control manner, control cycle of attitude control engine, ignition logic, startup control game of attitude control engine, etc. was researched
摘要對採用燃氣動力（直接力）與氣動力復合控制技術的控制方式、姿控發動機控制周期、點火邏輯及姿控發動機啟控策略等進行了初步探討。 -
The work module of rudder was discussed and studied by simulation in side jet and aerodynamic compound control manner, the effect on guidance accuracy by control cycle of attitude control engine and action cycle of control loop was simulated
重點對採用燃氣動力氣動力復合控制方式中舵系統的工作模式進行了探討及模擬研究，對姿控發動機控制周期及控制迴路工作周期對制導精度的影響進行了初步模擬研究。 -
( 2 ) to evaluate the effects of a reaction control jet on the aerodynamic performance of a missile operating at supersonic / hypersonic flight condition, the single and two attitude jet - interaction flow between a lateral jet and the external flow has been analyzed by detailed numerical simulation
（ 2 ）分別計算了單噴流和雙噴流干擾流場。詳細分析了流場結構和彈體表面壓力分佈特性，獲得了一些有實用價值的結果。 -
Designed semi - physical simulations emphasized on attitude determination algorithm based on star sensor combined with gyroscope, bang - off - bang time - optimal jet control algorithm, and quaternion feedback control algorithm using flywheel
重點針對星敏感器和速率陀螺聯合定姿演算法、噴氣bang - off - bang時間最優控制律演算法、反作用飛輪四元數反饋穩態控制律演算法分別設計了半物理模擬實驗。 -
At present, the most effective method of destroying the warhead of btm is the technology of directly hit kinetic kill, which can achieve precision control to the missile by adding the trajectory - control jet or attitude - control jet
目前對付來襲tbm彈頭最有效的手段就是採用直接碰撞動能殺傷技術。它是通過在導彈上安裝響應快速的雙組元軌、姿控發動機以實現對導彈的精確控制。 -
Lateral jet control technology is researched in this dissertation, based on supersonic / hypersonic missile aerodynamics and lateral jet interaction ( ji ) effects associated with the attitude control solid - propellant rocket motors system in the low endoatmospheric range
橫向噴流干擾效應研究在超聲速高超聲速導彈總體設計和精確制導技術研究領域一直佔有重要地位。本論文針對大氣層內超聲速高超聲速導彈採用姿態固體火箭發動機側噴流控制技術的一些問題進行了研究。 -
And then based on a surface - to - air missile that satisfies the requisition nearly, by means of reconstructing its geometry size, subsystems such as engine, the interceptor model used to continue the following studies is established. then the trajectory - control jet or attitude - control jet is added to the interceptor based on the analysis of the relationship between the missile performance and the thrust and configuration of the side jet
然後以基本滿足方案要求的某型防空導彈為基礎，對其幾何尺寸、發動機等分系統進行改進，並通過分析導彈性能與側噴發動機參數之間的關系，增加了姿控或軌控側向裝置，這樣得到了本文的研究工作所需的導彈模型。 -
C. based on a lot of referenced documents and tunnel experiment data, the phenomenon of lateral jet interception are analyzed, and the diagrams of the interaction factor " kcn " is presented. following, the airdefence missile model, trajectory model including attitude - control direct lateral force are constructed
3 、根據大量參考文獻和試驗數據，分析了側向噴流的干擾特性，並給出不同狀況下干擾因子k _ （ cn ）的變化曲線，在上述工作的基礎上，建立了帶有姿控側向力裝置的防空導彈模型和彈道計算模型。 -
In the case of jet engine not working, direct lateral force / attitude compound control system becomes only aerodynamic control system
當噴流發動機不工作時，直接力氣動力復合控制就變成了單獨的氣動力控制。 -
In the case of jet engine working, coupling ravel of direct lateral force / attitude compound control was realized
當噴流發動機工作時，對直接力氣動力復合控制實現了解耦。
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