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A fast-time study on increasing the capacity of continuous descent approaches through airborne precision spacing

机译:通过机载精密间隔提高连续下降能力的快速研究

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摘要

Due to projectedincrea ses in air traffic, there are several research efforts underwayto evaluate ways to safely increase the capacity of the National Airspace System(NAS), improve operational efficiency, andre duce aircraft noise. At NASA LangleyResearch Center (LaRC) in Hampton, Virginia, two parallel research efforts have focusedonterminal area research: one is Airborne Precision Spacing (APS), and theother is the Quiet Aircraft Technologies (QAT) project. The APS objective is toincrease terminal-area capacity without adversely affecting safety, whereas the QATproject objective is to develop noise- and fuel-efficient approach trajectories.The APS project developed a cockpit tool, called Airborne Merging and Spacingfor Terminal Arrivals (AMSTAR), that issues speedco mmands to aircraft to maintaindesired spacing between aircraft pairs. The APS studies showed an ability toincrease runway capacity; however, capacity increases may negatively impact noiseandemissio n levels in airport areas. The QAT project created efficient ContinuousDescent Approaches (CDAs), which showedred uctions in aircraft ground noise andfuel consumption. Previous research has shown that CDA trajectories have adverseeffects on runway capacity because aircraft must be spacedf urther apart at long distancesfrom the runway to prevent separation losses at the runway threshold. Todate, the APS and CDA concepts have been evaluated independently at LaRC.In this study, three different approaches to combining APS and CDA operationswere evaluatedto determine the feasibility and benefits of combining these concepts.These methods combined AMSTAR with 3◦-flight-path-angle-CDA approach routes,3◦-CDA routes with spoilers, and2 ◦-CDA routes without spoilers. Adding the useof spoilers allowedf aster responses to large speedr eductions issued by AMSTAR.This improvement was contrastedwith the effects of a shallower flight-path angle forgreater deceleration capabilities.This research indicated that AMSTAR improved the performance of CDA operations,although full capacity improvements were not achieved. Whereas the 2◦-CDAroutes were expectedto show the best results, the 3◦-CDA case with spoilers showedthe least variability in thresholdspacing errors. All of the CDA routes were morenoise, fuel, and time efficient than traditional step-descent routes that are commonlyusedto day.
机译:由于空中交通的预计增加,正在进行一些研究工作,以评估安全增加国家空域系统(NAS)容量,提高运行效率并减少飞机噪音的方法。在弗吉尼亚州汉普顿的NASA兰利研究中心(LaRC),两项并行的研究工作集中在航站区研究上:一项是机载精密间距(APS),另一项是“安静飞机技术”(QAT)项目。 APS的目标是在不影响安全的前提下增加码头区域的容量,而QAT项目的目标是开发噪音和燃油效率更高的进场轨迹。APS项目开发了一种驾驶舱工具,称为终端到达机载合并和间隔(AMSTAR),向飞机发出Speedco指令,以维持飞机对之间的期望间距。 APS研究表明可以增加跑道容量。但是,运力增加可能会对机场区域的噪声和发射水平产生负面影响。 QAT项目创建了有效的连续下降方法(CDA),该方法证明了飞机地面噪声和燃油消耗的作用。先前的研究表明,CDA轨迹会对跑道容量产生不利影响,因为飞机必须与跑道保持更长的距离,以防止在跑道入口处出现分离损失。迄今为止,APS和CDA概念已在LaRC上进行了独立评估。在这项研究中,我们评估了将APS和CDA操作相结合的三种不同方法,以确定将这些概念相结合的可行性和益处。这些方法将AMSTAR与3°-flight-path-角CDA进近路线,带扰流板的3◦-CDA路线和不带扰流板的2◦-CDA路线。增加扰流板的使用可以使AMSTAR发出的更大的速度响应更快,这一改进与较浅的飞行路径角对更大的减速能力产生的影响形成了鲜明的对比。该研究表明AMSTAR改进了CDA作业的性能,尽管没有充分提高产能实现。预期2◦-CDA路线将显示最佳结果,而3◦-CDA带有扰流板的情况显示阈值间距误差的可变性最小。与今天通常使用的传统逐步下降路线相比,所有CDA路线均具有更高的噪声,燃油效率和时间效率。

著录项

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    Weitz Lesley Anne;

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  • 年度 2005
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