今年年底从零到无限将开发一个规格的bloon系统，来测试整个的飞行周期。
Zero2infinity will be launching a scale version of bloon system later this year to test the entire cycle of the flight.
对单个飞行周期内地面目标的绝对高程精度与系统状态参数之间的关系进行了详细分析。
The calculation and simulation programs were also developed. The relations between the ground targets' absolute altitude and system parameters in a single flight period were analyzed in detail.
分析了地形匹配周期对飞行轨迹的影响。
The effect of terrain matching period to the flying procedure is analyzed.
商业飞行员学习周期在10 - 12个月，我们便可把您从零培训到可操作多引擎飞机的商业飞行员。
Commercial pilot learning cycle in 10-12 months, we can take you from zero training to operate a commercial pilot multi-engine airplanes.
其他的研究表明，睡眠不足，长时间的工作和身体自然周期的紊乱会干扰司机和飞行员的表现。
Other studies have shown that lack of sleep, prolonged work hours and natural body-rhythm disturbances reduce the performance of drivers and pilots.
在研发周期相同的阶段，我们的飞行时数和使用的飞机都要少得多，但我们的研究要更为深入，因为我们更有经验了，工具也更强大了。
We have fewer flying hours and fewer planes at an equivalent point in the development cycle but we are further along because we have more experience and better tools.
在正弦风切变假定下，利用计算机计算和飞行模拟器模拟研究了长周期振动频率上下的正弦波风切变对飞机着陆航迹的影响。
On the assumption that the wind shear is sinusoidal, the effects of long periodic oscillation on the landing path of an aircraft were studied by computer calculation and with flight simulator.
该系统对飞机实施全权限数字电传操纵，可以在飞行中改变飞机的操纵感觉特性、操纵系统特性和纵向短周期气动特性。
The system adopts full authority DFBW for aircraft, which may change the characteristics of control feel, handling system and longitudinal short-period aerodynamics during flight.
为缩短飞行指挥员的训练周期，提高训练效率，降低训练成本，设计并实现了基于PC的飞行指挥训练系统。
In order to improve the level of training flight commander, improve training efficiency, reduce training costs, the "PC-based training of the simulator of flight command system" was developed.
第一部分介绍飞行器实测振动数据的平稳性、周期性和正态性检验的几种方法；
The first deals with several i methods used to test stationarity, periodicity and guassianity of the recorded data of aircraft vibration.
研究了编队飞行的控制系统结构和共线拉格朗日点附近的周期轨道保持控制问题。
Secondly, the control system structure and station keeping problems near collinear Lagrange points are studied.
研究了有动力通用再入飞行器的燃料最优巡航轨迹，将问题转化为求解最优稳态巡航轨迹和最优周期巡航轨迹问题。
The fuel optimal cruise trajectory of a powered common aero vehicle was analyzed. The problem was divided into determining the optimal steady-state cruise and optimal periodic cruise problems.
研究了有动力通用再入飞行器的燃料最优巡航轨迹，将问题转化为求解最优稳态巡航轨迹和最优周期巡航轨迹问题。
The fuel optimal cruise trajectory of a powered common aero vehicle was analyzed. The problem was divided into determining the optimal steady-state cruise and optimal periodic cruise problems.
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