lateral attitude 中文意思是什麼
lateral attitude
解釋
橫向位置-
The main works and achievements are described : ( 1 ) the application of direct lateral force on the exoatmosphere kinetic - kill vehicle. at first, the collectivity project of the exoatmosphere kinetic - kill vehicle is specified, the motive model of the exoatmosphere kinetic - kill vehicle and target are constructed, and the thrust performance of trajectory - control engine and attitude - control engine are presented
研究的內容及成果主要表現在以下幾個方面： （一）直接側向力在大氣層外動能攔截器中的應用首先確定了動能攔截器的總體方案，分別建立目標運動和動能攔截器運動的數學模型，以及軌控和姿控發動機的推力模型。 -
( 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。 -
Among different movement mode of moving mass, the influence of lateral displacement of the moving mass on the attitude motion of the re - entry vehicle is discussed, the effect of different moving mass ratio and axis position imposing on the attitude of the reentry vehicle is also studied
本論文詳細地分析了影響系統姿態的因素，研究了在不同的質量體運動形式下，活動質量體的橫向偏移量、質量比、和軸向位置對姿態動力學響應的影響。 -
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。 -
The main works of this thesis are research of lateral force control and guidance of interceptors, emphasized on the terminal phase when intercepting the tactical ballistic missiles, including the performance analysis of extra - atmospheric kinetic - kill vehicle piloted by trajectory - control and attitude - control systems, and combined control of aerodynamics with lateral jets in atmosphere
本文主要研究攔截彈在攔截戰術彈道導彈時，末段的制導和側向力控制問題，包括大氣層外動能攔截器在姿控與軌控發動機作用下的性能分析，和大氣層內側向力與氣動力復合控制研究。 -
Side thrusters names : front thrusters are retro thrusters ; top / bottom thrusters are attitude thrusters ; left / right thrusters are lateral thrusters
側推進器名稱：前推進器為「制動推進器」 ；上/下推進器為「姿態推進器」 ：左/右推進器為「橫向推進器」 。 -
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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