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A new airborne tandem platform for collocated measurements of microphysical cloud and radiation properties

机译:一个新的机载串联平台,用于并置测量微物理云和辐射特性

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摘要

A new airborne tandem measurement platform for cloud-radiation interactionstudies is introduced in this paper. It consists of a Learjet 35A researchaircraft and the AIRcraft TOwed Sensor Shuttle (AIRTOSS), which is aninstrumented drag-body towed by the Learjet. Currently, the AIRTOSS isinstrumented with a Cloud Imaging Probe (CIP) for measuring cloudmicrophysical properties and an Inertial Navigation System (INS) formeasurements of flight attitudes. The cable dragging AIRTOSS can be as longas four kilometres. Thus, truly collocated measurements in two altitudesabove, in, and below clouds can be obtained. Results from first test flightswith Learjet and AIRTOSS are reported here. The flights were performed fromHohn Airport, Germany. Specific manoeuvres were flown to test the aerodynamicbehaviour of the drag-body and to investigate the suitability of AIRTOSS forhigh-precision irradiance measurements which require a stable flight attitudeof AIRTOSS. The flight attitude data show that AIRTOSS is sensitive toseveral flight manoeuvres such as turns, altitude and airspeed changes, andalso to changes of towing cable length. The effects of these manoeuvres onthe attitude angles of AIRTOSS have been quantified. Maximum roll angledeviations were observed during turns. Even small changes in headingcan lead to high roll angles (one degree change in heading causes a change inroll angle of about eight degrees). The pitch angle varies during climb ordive periods, extending or retracting of towing cable, acceleration ordeceleration, and even when flying at too low or too high true airspeeddepending on altitude. Values of pitch angle between −5° (dive) and8° (climb and retracting towing cable) have been observed. Whilechange in attitude is not problematic for cloud particle propertymeasurements it is for radiation measurements. Here, the deviation from thehorizontal should be no more than 3° to avoid large errors. Whenkeeping the above mentioned flight parameters constant, sufficiently stableflight conditions can be maintained to perform high-quality irradiancemeasurements with AIRTOSS in future experiments. During this test campaignalso observations of cloud microphysical data as for example droplet numberconcentrations and size distributions with the AIRTOSS in stratocumulusclouds were performed to prove the compliance with scientific needs.Simultaneous spectral cloud radiation measurements have been made. Themeasurements of internal operational data of AIRTOSS as well as the firstatmospheric data demonstrate the suitability of this tandem platform fordetailed cloud microphysics and radiation interaction studies.
机译:介绍了一种新的云辐射相互作用的机载串联测量平台。它由Learjet 35A研究飞机和AIRcraft拖曳传感器航天飞机(AIRTOSS)组成,后者是由Learjet拖曳的仪表拖曳体。当前,AIRTOSS配备了用于测量云微物理特性的云成像探头(CIP)和用于测量飞行姿态的惯性导航系统(INS)。拖曳AIRTOSS的电缆最长可达四公里。因此,可以获得在云层之上,之下和之下的两个高度的真正并置的测量值。此处报告了使用Learjet和AIRTOSS进行的首次试飞的结果。这些飞行是从德国霍恩机场进行的。进行了特定的操作以测试阻力体的空气动力学性能,并研究AIRTOSS是否适用于需要稳定的AIRTOSS飞行姿态的高精度辐照度测量。飞行姿态数据表明,AIRTOSS对转弯,高度和空速变化以及拖曳电缆长度的变化等多种飞行动作都很敏感。这些动作对AIRTOSS姿态角的影响已被量化。在转弯期间观察到最大侧倾角偏差。甚至很小的航向变化也会导致高侧倾角(航向变化1度会导致侧倾角变化约8度)。俯仰角在爬升或下潜期间,拖曳电缆的延伸或缩回,加速或减速以及甚至在根据真实高度以太低或太高的真实空速飞行时也会变化。观察到的俯仰角介于-5°(俯冲)和8°(爬升和后退拖缆)之间。虽然姿态变化对于云粒子特性测量而言并不成问题,但对于辐射测量而言却不成问题。在此,与水平方向的偏差应不超过3°,以避免大的误差。当保持上述飞行参数不变时,可以保持足够稳定的飞行条件,以在将来的实验中使用AIRTOSS进行高质量的辐照度测量。在该测试活动中,还观察了云的微物理数据,例如平流云中的AIRTOSS观测到的液滴数量浓度和大小分布,以证明其符合科学需要。同时进行了光谱云辐射测量。 AIRTOSS的内部运行数据以及第一个大气数据的测量证明了该串联平台适用于详细的云微物理学和辐射相互作用研究。

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