175 research outputs found
Airborne lidar observations supporting the ADM-Aeolus mission for global wind profiling
The Atmospheric Dynamics Mission ADM-Aeolus of
ESA will be the first lidar mission to sense the global
wind field from space. The instrument is based on a
direct-detection Doppler lidar operating at 354.9 nm
with two spectrometers for aerosol/cloud and molecular
backscatter. In order to assess the performance of the
Doppler lidar ALADIN on ADM-Aeolus and to
optimize the retrieval algorithms with atmospheric
signals, an airborne prototype â the ALADIN Airborne
Demonstrator A2D â was developed. The A2D was the
first airborne direct-detection Doppler lidar with its
maiden flight on the DLR Falcon aircraft in 2005.
Three airborne campaigns with a coherent-detection
2-ÎŒm wind lidar and the direct-detection wind lidar
A2D were performed for pre-launch validation of
Aeolus from 2007-2009. Furthermore, a unique
experiment for resolving the Rayleigh-Brillouin
spectral line shape in the atmosphere was accomplished
in 2009 with the A2D from a mountain observatory at
an altitude of 2650 m. Results of this experiment and
the latest airborne campaign in the vicinity of
Greenland and Iceland will be discussed
Die StÀdte des Herzogtums Kleve und ihre Beziehungen zum lÀndlichen Raum im 18. Jahrhundert (1713 - 1806)
Die vorliegende Arbeit versucht, am Beispiel des Herzogtums Kleve die Entwicklung der Raumbeziehungen vorindustrieller StĂ€dte unter dem preuĂischen Absolutismus garzulegen. Gerade dieses preuĂische Nebenterritorium mit seiner aus dem Mittelalter herrĂŒhrenden StĂ€dtelandschaft ist geeignet, die Wirkungen der raumwirksamen StaatstĂ€tigkeit des friderizianischen PreuĂens auf das GefĂŒge der Stadt-Land-Beziehungen aufzuzeigen. Eine solche Arbeit muĂ zwangslĂ€ufig unvollstĂ€ndig bleiben. Sie kann die oben angesprochene Problematik nur schlaglichtartig beleuchten. Dies muĂ nicht zuletzt deshalb eingerĂ€umt werden, da wichtige raumbezogene Daten entweder unter den - im Vergleich zu heute â anders gearteten Intentionen vorindustrieller Statistik nicht erhoben wurden oder durch die Zerstörungen des zweiten Weltkrieges unwiederbringlich verlorengingen. Die weitgehende Vernichtung der BestĂ€nde des Emmericher Stadtarchivs (1945) sei hier als Beispiel genannt
Coupling multi-fluid dynamics equipped with Landau closures to the particle-in-cell method
The particle-in-cell (PIC) method is successfully used to study magnetized
plasmas. However, this requires large computational costs and limits
simulations to short physical run-times and often to setups in less than three
spatial dimensions. Traditionally, this is circumvented either via hybrid-PIC
methods (adopting massless electrons) or via magneto-hydrodynamic-PIC methods
(modelling the background plasma as a single charge-neutral
magneto-hydrodynamical fluid). Because both methods preclude modelling
important plasma-kinetic effects, we introduce a new fluid-PIC code that
couples a fully explicit and charge-conservative multi-fluid solver to the PIC
code SHARP through a current-coupling scheme and solve the full set of
Maxwell's equations. This avoids simplifications typically adopted for Ohm's
Law and enables us to fully resolve the electron temporal and spatial scales
while retaining the versatility of initializing any number of ion, electron, or
neutral species with arbitrary velocity distributions. The fluid solver
includes closures emulating Landau damping so that we can account for this
important kinetic process in our fluid species. Our fluid-PIC code is
second-order accurate in space and time. The code is successfully validated
against several test problems, including the stability and accuracy of shocks
and the dispersion relation and damping rates of waves in unmagnetized and
magnetized plasmas. It also matches growth rates and saturation levels of the
gyro-scale and intermediate-scale instabilities driven by drifting charged
particles in magnetized thermal background plasmas in comparison to linear
theory and PIC simulations. This new fluid-SHARP code is specially designed for
studying high-energy cosmic rays interacting with thermal plasmas over
macroscopic timescales.Comment: 35 pages, 11 figures, submitted to JPP. Comments are welcom
Deciphering the physical basis of the intermediate-scale instability
We study the underlying physics of cosmic-ray (CR) driven instabilities that
play a crucial role for CR transport across a wide range of scales, from
interstellar to galaxy cluster environments. By examining the linear dispersion
relation of CR-driven instabilities in a magnetised electron-ion background
plasma, we establish that both, the intermediate and gyroscale instabilities
have a resonant origin and show that these resonances can be understood via a
simple graphical interpretation. These instabilities destabilise wave modes
parallel to the large-scale background magnetic field at significantly distinct
scales and with very different phase speeds. Furthermore, we show that
approximating the electron-ion background plasma with either
magnetohydrodynamics (MHD) or Hall-MHD fails to capture the fastest growing
instability in the linear regime, namely the intermediate-scale instability.
This finding highlights the importance of accurately characterising the
background plasma for resolving the most unstable wave modes. Finally, we
discuss the implications of the different phase speeds of unstable modes on
particle-wave scattering. Further work is needed to investigate the relative
importance of these two instabilities in the non-linear, saturated regime and
to develop a physical understanding of the effective CR transport coefficients
in large-scale CR hydrodynamics theories.Comment: 14 pages, 3 figures, submitted to JPP Letters, comments welcom
ADM-Aeolus pre-launch activities and recent advances in spaceborne and airborne Wind Lidar Systems
The first space-borne wind lidar mission ADM-Aeolus from ESA is currently scheduled for launch by mid-2017. For the preparation of the Aeolus validation, an airborne field experiment was performed during 3 weeks in May 2015 with the DLR Falcon and the NASA DC-8 aircraft. For the first time 4 wind lidars were deployed during an airborne campaign including two coherent and two direct-detection wind lidars at a wavelength of 2ÎŒm and 355 nm. A total of 7 coordinated flights of the Falcon and DC-8 yielded an extensive dataset.
Additionally, DLRâs airborne coherent Doppler Wind Lidar was recently deployed in 3 coordinated airborne campaigns aiming to investigate the life cycle of gravity waves from ground up to the mesosphere. The horizontal and vertical wind measurements of the lidar provide valuable data for characterizing tropospheric gravity waves and background wind conditions
Quality control and error assessment of the Aeolus L2B wind results from the Joint Aeolus Tropical Atlantic Campaign
Since the start of the European Space Agency's Aeolus mission in 2018, various studies were dedicated to the evaluation of its wind data quality and particularly to the determination of the systematic and random errors in the Rayleigh-clear and Mie-cloudy wind results provided in the Aeolus Level-2B (L2B) product. The quality control (QC) schemes applied in the analyses mostly rely on the estimated error (EE), reported in the L2B data, using different and often subjectively chosen thresholds for rejecting data outliers, thus hampering the comparability of different validation studies. This work gives insight into the calculation of the EE for the two receiver channels and reveals its limitations as a measure of the actual wind error due to its spatial and temporal variability. It is demonstrated that a precise error assessment of the Aeolus winds necessitates a careful statistical analysis, including a rigorous screening for gross errors to be compliant with the error definitions formulated in the Aeolus mission requirements. To this end, the modified Z score and normal quantile plots are shown to be useful statistical tools for effectively eliminating gross errors and for evaluating the normality of the wind error distribution in dependence on the applied QC scheme, respectively. The influence of different QC approaches and thresholds on key statistical parameters is discussed in the context of the Joint Aeolus Tropical Atlantic Campaign (JATAC), which was conducted in Cabo Verde in September 2021. Aeolus winds are compared against model background data from the European Centre for Medium-Range Weather Forecasts (ECMWF) before the assimilation of Aeolus winds and against wind data measured with the 2â”m heterodyne detection Doppler wind lidar (DWL) aboard the Falcon aircraft. The two studies make evident that the error distribution of the Mie-cloudy winds is strongly skewed with a preponderance of positively biased wind results distorting the statistics if not filtered out properly. Effective outlier removal is accomplished by applying a two-step QC based on the EE and the modified Z score, thereby ensuring an error distribution with a high degree of normality while retaining a large portion of wind results from the original dataset. After the utilization of the described QC approach, the systematic errors in the L2B Rayleigh-clear and Mie-cloudy winds are determined to be below 0.3âmâsâ1 with respect to both the ECMWF model background and the 2â”m DWL. Differences in the random errors relative to the two reference datasets (Mie vs. model is 5.3âmâsâ1, Mie vs. DWL is 4.1âmâsâ1, Rayleigh vs. model is 7.8âmâsâ1, and Rayleigh vs. DWL is 8.2âmâsâ1) are elaborated in the text.</p
Verification of different Fizeau fringe analysis algorithms based on airborne wind lidar data in support of ESA's Aeolus mission
The Aeolus mission by the European Space Agency was launched in August 2018 and stopped operations in April 2023. Aeolus carried the direct-detection Atmospheric LAser Doppler INstrument (ALADIN). To support the preparation of Aeolus, the ALADIN Airborne Demonstrator (A2D) instrument was developed and applied in several field campaigns. Both ALADIN and A2D consist of so-called Rayleigh and Mie channels used to measure wind from both molecular and particulate backscatter signals. The Mie channel is based on the fringe-imaging technique, which relies on determining the spatial location of a linear interference pattern (fringe) that originated from multiple interference in a Fizeauspectrometer.The accuracy of the retrieved winds is among others depending on the analytic algorithm used for determining the fringe location on the detector. In this paper, the performance of two algorithms using Lorentzian and Voigt fit functions is investigated by applying them to A2D data that were acquired during the AVATAR-I airborne campaign. For performance validation, the data of a highly accurate heterodyne detection wind lidar (2-”m DWL) that was flown in parallel are used as a reference. In addition, a fast and non-fit-based algorithm based on a four-pixel intensity ratio approach (R4) is developed. It is revealed that the Voigt-fit-based algorithm provides 50% more data points than the Lorentzian-based algorithm while applying a quality control that yields a similar random error of about 1.5 m/s. The R4 algorithm is shown to deliver a similar accuracy as the Voigt-fit-based algorithms, with the advantage of a one to two orders of magnitude faster computation time. Principally, the R4 algorithm can be adapted to other spectroscopic applications where sub-pixel knowledge of the location of measured peak profiles is needed
RAYLEIGH WIND RETRIEVAL FOR THE ALADIN AIRBORNE DEMONSTRATOR OF THE AEOLUS MISSION USING SIMULATED RESPONSE CALIBRATION
Aeolus, launched on 22 August 2018, is the first ever satellite to directly observe wind information from space on a global scale. An airborne prototype called ALADIN Airborne Demonstrator (A2D) was developed at the German Aerospace Center (DLR) for validating the Aeolus measurement principle based on realistic atmospheric signals. However, atmospheric and instrumental variability currently limit the reliability and repeatability of the A2D instrument response calibration. In this study, a simulated Rayleigh response calibration (SRRC) is presented for resolving the limitations of A2D instrument response calibration
Airborne temperature profiling in the troposphere during daytime by lidar utilizing RayleighâBrillouin scattering
The airborne measurement of a temperature profile from 10.5 km down towards ground (about 1.4 km above sea level) during daytime by means of a lidar utilizing Rayleigh-Brillouin (RB) scattering is demonstrated for the first time, to our knowledge. The spectra of the scattered light were measured by tuning the laser (Lambda=354.9 nm) over a 11 GHz frequency range with a step size of 250 MHz while using a Fabry Perot interferometer as a spectral filter. The measurement took 14 min and was conducted over a remote area in Iceland with the ALADIN Airborne Demonstrator on-board the DLR Falcon aircraft. The temperature profile was derived by applying an analytical RB line shape model to the backscatter spectra, which were measured at different altitudes with a vertical resolution of 630 m. A comparison with temperature profiles from radiosonde observations and model temperatures shows reasonable agreement with biases of less than +/-2K. Based on Poisson statistics, the random error of the derived temperatures is estimated to vary between 0.1 K and 0.4 K. The work provides insight into the possible realization of airborne lidar temperature profilers based on RB scattering
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