dual flight 中文意思是什麼
dual flight
解釋
帶飛-
The delta-winged columbia, before reaching the orbit, jettisoned its dual booster rockets two minutes into flight.
三角翼的哥倫比亞號航天飛機在進入軌道前，起飛兩分鐘就拋下其兩個助推火箭。 -
The paper studies the project of improving the reliability of flight control computer by using the dual cpu hot - redundancy technology
本文主要對利用雙機熱備份技術來提高飛控計算機可靠性這一方案進行了前期研究。 -
The method can be used for many flight control computers easily. the dual cpu hot - redundancy technology became a method to improve the reliability of flight control computer
該方法實施簡單，易移植和工程化，具有較好的通用性，為提高飛控計算機可靠性提供了一種途徑。 -
We implement the dual cpu hot - redundancy technology into the common uav which used pc / 104 in our country. the reliability of flight control computer can be improved rapidly only if we increase a little hardware and software by the dual cpu hot - redundancy technology
該技術在我國無人機普遍使用的pc 104體系結構作為平臺的飛控計算機上實施，只需增加少量的硬體資源和軟體模塊就可以大大提高飛控計算機的可靠性。 -
Firstly discussing basic type of computer redundant structure and characteristic of the systems, the self - monitoring dual redundancy computer systems is brought forward as the design scheme for the required flight control computer system. the redundant structure is researched about reliability by using markor model and is carefully designed
首先分析了計算機冗餘結構的基本類型以及本次設計的要求特點，選擇了自監控二冗餘飛行控制計算機系統的設計方案，運用馬爾科夫模型對此冗餘系統的可靠性進行了計算研究，並且對此冗餘結構進行了詳細地描述及設計。 -
Focusing on the flight control computer system of some type of airplane, this paper first analyzes the advantage and disadvantage of the structures of many kinds of fault tolerant flight control computer systems and their ability in tolerating fault, followed by summarizing the key design technology. the dual similar redundancy fault tolerant computer system is brought forward as the design scheme for the required flight control computer. also brought forward is the particular system design
本文以某型號飛機飛控計算機系統為研究對象，首先分析了各種類型容錯飛控計算機體系結構的優缺點及容錯能力，總結了容錯計算機系統設計的關鍵技術，然後提出了二模相似余度容錯飛控計算機系統設計方案，詳細設計了以motorola公司生產的先進powerpc740微處理器為核心處理器、以高性能的國際標準化通用vme總線為內總線的交叉通道通信容錯計算機系統。 -
In the range of flight mach number mo = 3 ~ 7, in order to take the advantage of ramjet and scramjet, a fix - shaped dual - mode scramjet, in which both subsonic and supersonic combustion can be obtained, is used for hypersonic vehicle
在飛行馬赫數m _ = 3 - 7的范圍內，為充分發揮沖壓發動機的性能優勢，高超聲速飛行器採用了既能在亞聲速燃燒模態，又能在超聲速燃燒模態下工作的固定幾何形狀的雙模態沖壓發動機。 -
There are great differences between ground test of a flight vehicle ' s aerodynamics and that of a dual - mode scramjet when ground test facilities are used to do experiments on a dual - mode scramjet engine, the components of incoming flow and its parameters, including total pressure, total temperature ( or total enthalpy ) and velocity must be simulated. at the same time, since the fuel ' s resident time within a combustor is very short, on the order of one millisecond, it is difficult to measure the flow - fields
進行雙模態沖壓發動機地面試驗研究時，必須要求試驗設備能模擬實際飛行條件下來流氣體的組分、總壓、總溫（或總焓）以及來流氣體的流動速度；同時由於燃料在燃燒室內駐留的時間很短，一般為毫秒量級，從而使流場物理量的測定顯得非常困難。 -
By means of dual - time stepping method and moving grids technique, we solved the 3 - d unsteady euler ' equations for helicopter rotor in forward flight, and obtained the near - field hsi noise
為了多槳旋翼旋轉、變距等復合運動的準確描述，採用了多塊分區運動網格技術。
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