高高原起飞推力限制参数验证飞行航迹研究

起飞推力限制参数验证试飞(lapse-rate take off,简称LRTO)是飞机高高原动力试飞的核心科目之一。该科目在高高原试飞时,需要在高高原机场的最低安全高度(minimum safety altitude,简称MSA)以下飞行。针对高高原起飞推力限制参数验证试飞的飞行航迹设计进行了研究。介绍了扇区最低安全高度的定义和CCAR91部对低高度飞行的适用条款。阐述了航迹设计的基本要求,包括保护区的定义和要求、航迹精度的构成。详细描述了低于扇区最低安全高度飞行航迹的设计方法,包括试飞区域地形数据的获取、航迹绘制的经验总结、航迹的性能校核、模拟机校核和真机飞行时的逐步逼近。以稻城亚丁机场为例介绍了设计完成的飞行航迹在稻城机场应用的情况,包括航迹在实际应用中的超障余度和应用时的气象要求。     

Variations in Electron Content Ratio and Semi-thickness Ratio during LSA and MSA periods and some Cyclone Genesis Periods using COSMIC satellite observations

In this study for the first time, COSMIC satellite data have been used to deduce values of ionospheric Electron Content Ratio (ECR) and Semi-thickness Ratio (Rtb) for Low Solar Activity (LSA) (2008) and Moderate Solar Activity (MSA) (2012) periods over the Indian low-latitude (15–30°N) region with 80–95°E longitude. These two ratios provide sensitive information about bottom and topside ionosphere for different geophysical conditions. Extraction of suspected patterns and discrepancies unfold that the deviations between ECR and Rtb values during LSA period are comparatively higher than that of MSA period when the diurnal variability in these two parameters is flatter along with the diurnal-dips during pre-noon hours. The correlative relationship of ECR exhibits low association with NmF2 and anti-correlation with HmF2, whereas its correlation with Rtb is extremely high. During Cyclone Genesis Period (CGP) strong dips in ECR and Rtb values with respect to pre and post CGP occurred which helps to take decisive conclusion about the ionospheric variations to be dominant through getting relatively higher Ne concentration in the bottom side part of the ionosphere.