A method in region deploying based on GA was proposed for the aerial refueling mission in threat existing environments.
对存在敌威胁时的空中加油任务，提出了一种基于遗传算法的区域配置方法。
The method this thesis presented could conveniently extend to the research of aerial refueling and air traffic security.
本文的研究方法可以方便的推广到空中加油以及空中交通安全的研究中。
The January flight was key to reducing risks as the program prepares for autonomous aerial refueling of two Global Hawks in the spring of 2012.
1月飞行测试的关键是减少KQ - X项目风险，为2012年春天进行的两架全球鹰无人机自主空中加油做好准备。
As military aviation moves toward the next century, aerial refueling will continue to provide the means to project military power to the far reaches of the globe.
在军事航空迈向新世纪的同时，空中加油将继续为向地球远方投送军事力量提供一种方式方法。
Military fuel facility, TT5000 monitors approximated 4500 feet of 12 "stainless steel hydrant piping used by Kansas Air National Guard for KC-135 Aerial Refueling Squadron."
军用燃料设施，TT 5000监控大约4500英尺的12号不锈钢消防管道。堪萨斯州空军国民警卫队用这些管道给航空燃料补给中队提供燃料。
The disturbances acting on the receiver aircraft in the docking phase of an aerial refueling are analyzed and the truth of longitudinal flight control of the receiver is introduced.
分析了空中加油对接过程中受油机受到的各种扰动，阐述了插头锥管加油方式受油机的纵向飞行控制原理。
It can fly more than 6, 000 nautical miles without refueling and more than 10, 000 nautical miles with just one aerial refueling, giving it the ability to reach any point on the globe within hours.
B - 2隐形机在没有加油的情况下，飞行距离能达11000km以上，仅加一次油，飞行距离能达18500 km以上，能够在一个小时内到达世界上任何一个地区。
The primary purpose of the KC-135 Stratotanker is aerial aircraft refueling for air Force, Navy, Marine Corps, and allied nations.
KC- 135“同温层加油机”主要用于为美空军、海军和海军陆战队及美国的盟军进行空中燃料补给。
The formation and distribution of wake flow behind a large aerial tanker are discussed, Then the mathematic model of disturbance to the refueled aircraft during refueling is given.
研究了大型授油机尾流的形成和分布特点，分析了受油机在不同位置进入黾流时飞机所受的影响，提出了相应的数学建模方法。
The formation and distribution of wake flow behind a large aerial tanker are discussed, Then the mathematic model of disturbance to the refueled aircraft during refueling is given.
研究了大型授油机尾流的形成和分布特点，分析了受油机在不同位置进入黾流时飞机所受的影响，提出了相应的数学建模方法。
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