Chinese translation for "牵引飞行"
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- aerotow flight
Related Translations:
机械牵引: mechanical tractionpower traction 牵引伞: extraction parachute 牵引复位: replacement by tractiontraction reduction 牵引板: pull bladetowing plate 牵引角: angle of draftangle of drawangle of hitchangle of pullangle of tractiondraught angle 牵引中断: zugunterbrechung drive interruption
- Example Sentences:
| 1. | Finally , one trajectory meeting the height and the speed of towing flight is designed
最终设计出一条满足牵引飞行高度和速度的轨道。 | | 2. | Utilize data processing method , two groups of data of the towed plane is compared
利用数据拟合方法，对计算数据进行比较，分析牵引飞行特性。 | | 3. | Making use of user " s module offered by vpm , write the emulation procedure of the towed flight
第三部分熟悉仿真框架软件vpm ，并利用vpm提供的用户模块编写牵引飞行仿真程序。 | | 4. | Through calculating and analyzing basic performance , the flight characteristic of the towed system is researched . stability and control issue of carrier rocket is discussed primarily . the net result of the thesis will prove the feasibility of the scheme of towed launch
论文通过牵引系统基本性能的计算和分析，完成牵引飞行特性的研究，同时对运载器的稳定性和控制问题进行初步的探讨，最终结果将验证牵引发射方案的可行性。 | | 5. | This paper relies on country 863 project " taking off levelly , two stage to orbit and transatmosphere flight vehicle system design " , research towed flight dynamics primarily , development for our country air launch technology of carrier rocket , offering the essential technological reserve
本论文以国家863项目“水平起飞两级入轨跨大气层飞行器总体设计”为依托，对牵引飞行动力学进行初步研究，为我国研究运载火箭空中发射技术提供必要的技术储备。 | | 6. | Have put forward the schemes of five kinds of setting - up models by analysis to towed flight , concrete course and basic theories of scheme carry on the simple narration on each , compare their pluses and minuses . combine with study the purpose , the suitable method towed systematic modeling way is chosen
通过对牵引飞行过程的分析，提出了五种建立模型的方案，就每种方案的基本理论以及建模过程进行简单的叙述，对它们的优缺点进行比较，结合研究目的选择出适合的方法作为牵引系统的建模方式。 | | 7. | According to purpose of the towed flight , a new trajectory consisting of taking off , climbing phase , level flight phase is presented with . trajectory pitch angle of the towing plane is optimized . according to the flight law of the towing plane , the fin deflection angle and amplification coefficient of particle - system trajectory of carrier rocket are designed , in order to realizing flight steadily of the carrier rocker
根据牵引飞行的目的，对载机应用了“起飞?爬升?平飞”的变轨道飞行方案，同时对载机轨道的倾角、倾角变化规律进行优选设计；再根据载机的飞行规律，对运载器质点系轨道的舵偏规律及其放大系数进行了设计计算，实现运载器稳定牵引飞行。 | | 8. | Secondly , towed system is considered as many rigid body systems . according to research approaches of many rigid body systematic dynamics , the towed systematic engagement calculating models is derived ; according to actual course of the towed flight , deriving mathematics model of the course of taking off and towed flight of the towing plane and of carrier rocket , and corresponding parameter calculate models
其次将牵引系统作为多刚体系统宋考虑，根据多刚体系统动力学研究方法，建立牵引系统约束方程，由此推导出约束力计算公式；根据牵引飞行实际过程，推导出载机、运载器在起飞阶段，巡航飞行阶段的数学模型，以及相应的参数计算模型。 |
- Similar Words：
- "牵引翻转犁绕纵轴翻转" Chinese translation, "牵引范围" Chinese translation, "牵引方式" Chinese translation, "牵引方向" Chinese translation, "牵引飞机" Chinese translation, "牵引复滑车" Chinese translation, "牵引复位" Chinese translation, "牵引负荷" Chinese translation, "牵引负载" Chinese translation, "牵引杆" Chinese translation
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