GEOS - 5模型在戈达德太空飞行中心新建的美国国家航空航天局气候模拟中心的“探索”超级计算机上运行，它拥有约15000个处理器，并且即将增加。
The GEOS-5 model runs on the Discover supercomputer in the new NASA Center for Climate Simulation at Goddard Space Flight Center. Discover contains nearly 15,000 processors and will soon be augmented.
典型的教练机训练效能计算模型对飞机的航空电子系统、操纵系统考虑不足，对飞行参数选择有局限性。
The typical computation model of training effectiveness of training plane has limitation in selection of flight parameters as well as insufficient attention to avionics and control system.
实验结果表明，该模型能客观地反映飞行程序安全性且有计算简便的特点。
The result indicates that these models can express quantitative index for flight procedures′ safety correctly and objectively, and the calculation methods are simple and convenient.
主要介绍了应用最优过程理论计算飞机最优飞行轨迹的数学模型和计算方法。
It is introduced that the application of optimum process theory to flight trajectory optimization. In this paper, it has studied the method of dealing with changing parameter.
最后采用算例直升机数据，进行了定直飞行的配平计算和操纵响应分析，结果证明了模型的合理性和有效性。
Finally the trim calculation and response analysis are carried out with the example helicopter's data. The results validate the rationality and validity of the model.
此动力学模型可用于弹丸大攻角飞行时的弹道计算及某些灵巧弹药（如末敏弹）的设计。
This kinetic model can be used in ballistic calculation of projectile with large angle of attack and also in the design of some smart munitions(e. g. target sensitivity projectile).
它是生成三维立体地貌，计算地面距离、坡度、土方、面表积等的基础数据模型，也是巡航飞行器地形相关匹配的基础数据。
It is the basic model for various GIS operations, and the key data for terrain correlation matching of cruise missiles as well.
在进行亚音速气动分析时，应用线化速度势理论计算运载器的气动力系数，而后进行回归分析，得到运载器亚音速飞行时的气动特性模型。
For subsonic aerodynamic analysis, Linearized Velocity Potential Theory is used to evaluate the aerodynamic coefficient, and we can get subsonic aerodynamic model of vehicle by Regression analysis.
利用旋臂式模型机动飞行试验机进行倾转过渡状态下旋翼瞬态拉力的试验研究，试验与理论计算结果表现出很好的相关性。
The experiment of transient rotor thrust during transition flight has been carried out on whirling beam test facility, and the experimental results show excellent agreement with theory.
建立了飞行器、地形、地物的三维模型，利用计算出来的数据进行飞行器的实时三维视景仿真模拟。
The three dimension module of aircraft, terrain and object were erected, and real time three dimension visual simulation of was executed through computed data.
建立了飞行器、地形、地物的三维模型，利用计算出来的数据进行飞行器的实时三维视景仿真模拟。
The three dimension module of aircraft, terrain and object are erected, and real time three dimension visual simulation of is executed through computed data.
轨道计算主要用来模拟飞行器的飞行过程，前提是建立动力学模型。
The main function of orbit calculation is to simulate the flight procedure of spacecraft, before that, the dynamics model of orbit must be established.
利用人机工程学的理论和方法，采用中国飞行员人体数据，运用人体模型进行人机系统计算机仿真。
Utlizing the theory means of Ergonomics, we make use of the dummy, which is made based on Chinese pilots? Anthropometric data, to simulate the Human-Machine system.
该模型可计算不同过载谱、不同抗荷装备条件下的飞行员过载耐限和耐受时间。
It can be used to investigate G-Tolerance and duration time in different kinds of acceleration profiles and anti-G equipments.
所提出的计算模型、控制策略和分析方法适用于目标飞行器交会对接轨道设计和控制实施。
The proposed model, control strategy and analysis methods are applicable to the target′s rendezvous orbit design and control implementation.
根据此模型，对发动机性能进行了计算，进而计算出飞行性能。
The characters of the engine and the flying performance of the helicopter are calculated based on the thermodynamic math model.
将高速滑体制成相似的机翼模型，进行风洞试验，即可测定滑坡凌空飞行的空气动力学参数，从而计算大型高速滑坡凌空飞行的空气动力升力、飞行速度和飞行距离等。
If we make a wing model which is similar to sliding mass, we can determine aerodynamic parameters by the wind tunnel testing and thus calculate the lift.
对某飞船返回舱的飞行试验数据进行了计算和分析，结果证实了弹道重建数学模型的正确性和算法的可行性。
The flight test data of some a reentry capsule are analyzed. The results validate the developed mathematical model and algorithm of trajectory reconstruction.
对某飞船返回舱的飞行试验数据进行了计算和分析，结果证实了弹道重建数学模型的正确性和算法的可行性。
The flight test data of some a reentry capsule are analyzed. The results validate the developed mathematical model and algorithm of trajectory reconstruction.
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