依据拖曳系统的耦合特性和约束条件，建立了拖曳飞行动力学和运动学方程，提出了一种基于仿真的拖曳系统飞行性能计算方法。
According to the coupling characteristics and constrained conditions of the towing system, the models of dynamics and kinematics of the towing system were built up.
并以某小型涡喷发动机为例，沿飞行轨迹计算分析了射流预冷却对发动机性能的影响。
Taking the certain small scaled turbojet as an example, the influence by mass injection and pre-cooled engine was calculated and analyzed along fly trajectory.
根据计算结果对其所处的稀薄区域和稀薄效应对磁头飞行性能的影响进行了分析和讨论。
According to the calculated results, discussions and analyses are then presented to reveal the effects of rarefied region and rarefied effect on the working performances of the magnetic head.
通过算例计算了各种干扰及目标RCS对飞行器隐身性能的影响。
They were discussed the influence of various type of jamming and RCS on the stealth performance.
通过算例计算了箔条干扰及目标RCS对飞行器隐身性能的影响。
Some examples, which calculated the impact of chaff and RCS of targets on stealth performance, were given.
微型飞行器是集航空设计、航空制造、微机械、电子、高性能数字计算机于一体的多学科交叉的综合系统。
Micro air vehicle is a multidisciplinary system which integrates the technologies of aeronautical design, aeronautical manufacture, micro machinery, electronics and high capability digital computer.
按照高性能和小型化的要求，设计并实现了基于DSP的新型无人机飞行控制计算机硬件的设计和开发。
According to the high performance and the miniaturized request, designed and has realized based on the DSP new unmanned aerial vehicle flight control computer hardware's design and the development.
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.
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.
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