Ground calibration results of the JUICE ultraviolet spectrograph

Author(s):  
Michael W. Davis ◽  
G. R. Gladstone ◽  
Rohini S. Giles ◽  
Thomas K. Greathouse ◽  
Philippa M. Molyneux ◽  
...  
Keyword(s):  
2019 ◽  
Vol 71 (1) ◽  
Author(s):  
Bin Zhou ◽  
Bingjun Cheng ◽  
Xiaochen Gou ◽  
Lei Li ◽  
Yiteng Zhang ◽  
...  

Abstract The High Precision Magnetometer (HPM) is one of the main payloads onboard the China Seismo-Electromagnetic Satellite (CSES). The HPM consists of two Fluxgate Magnetometers (FGM) and the Coupled Dark State Magnetometer (CDSM), and measures the magnetic field from DC to 15 Hz. The FGMs measure the vector components of the magnetic field; while the CDSM detects the magnitude of the magnetic field with higher accuracy, which can be used to calibrate the linear parameters of the FGM. In this paper, brief descriptions of measurement principles and performances of the HPM, ground, and in-orbit calibration results of the FGMs are presented, including the thermal drift and magnetic interferences from the satellite. The HPM in-orbit vector data calibration includes two steps: sensor non-linearity corrections based on on-ground calibration and fluxgate linear parameter calibration based on the CDSM measurements. The calibration results show a reasonably good stability of the linear parameters over time. The difference between the field magnitude calculated from the calibrated FGM components and the magnitude directly measured by the CDSM is just 0.5 nT (1σ) when the linear parameters are fitted separately for the day- and the night-side. Satellite disturbances have been analyzed including soft and hard remanence as well as magnetization of the magnetic torquer, radiation from the Tri-Band Beacon, and interferences from the rotation of the solar wing. A comparison shows consistency between the HPM and SWARM magnetic field data. Observation examples are introduced in the paper, which show that HPM data can be used to survey the global geomagnetic field and monitor the magnetic field disturbances in the ionosphere.


2020 ◽  
Vol 187 ◽  
pp. 104923
Author(s):  
N.P.S. Mithun ◽  
Santosh V. Vadawale ◽  
M. Shanmugam ◽  
Arpit R. Patel ◽  
Nishant Singh ◽  
...  

Author(s):  
Maurice A. Leutenegger ◽  
Gregory V. Brown ◽  
Meng P. Chiao ◽  
Daniel Haas ◽  
Jan-Willem A. den Herder ◽  
...  
Keyword(s):  
X Ray ◽  

2016 ◽  
Vol 9 (3) ◽  
pp. 1279-1301 ◽  
Author(s):  
Rosemary Munro ◽  
Rüdiger Lang ◽  
Dieter Klaes ◽  
Gabriele Poli ◽  
Christian Retscher ◽  
...  

Abstract. The Global Ozone Monitoring Experiment-2 (GOME-2) flies on the Metop series of satellites, the space component of the EUMETSAT Polar System. In this paper we will provide an overview of the instrument design, the on-ground calibration and characterization activities, in-flight calibration, and level 0 to 1 data processing. The current status of the level 1 data is presented and points of specific relevance to users are highlighted. Long-term level 1 data consistency is also discussed and plans for future work are outlined. The information contained in this paper summarizes a large number of technical reports and related documents containing information that is not currently available in the published literature. These reports and documents are however made available on the EUMETSAT web pages and readers requiring more details than can be provided in this overview paper will find appropriate references at relevant points in the text.


Author(s):  
Megan E. Eckart ◽  
Joseph S. Adams ◽  
Kevin R. Boyce ◽  
Gregory V. Brown ◽  
Meng P. Chiao ◽  
...  
Keyword(s):  
X Ray ◽  

2013 ◽  
Vol 694-697 ◽  
pp. 1068-1073
Author(s):  
Jie Duan ◽  
Zhi Yong An ◽  
Xiang Yang Sun

In order to meet the high precision calibration requirements of precision angular distance and high magnitude to the optical navigation sensor, A new style of high precision star simulator with large caliber, and long-focus, is presented. And then the main compositions of this simulator are designed in detail referring to the simulator, the steering mirror, the standard simulated targets and so on. According to the simulator characteristics of large size lens and multi lens, the structural of lens cone uses the tube sleeve and inner sleeves fixed together means. To eliminate the mirror deformation, the design plan based on the tiny stress is applied in steering mirror. In order to achieve a high magnitude, the light targets are simulated by optical transmission from OLED to high precision drone with fibers. Its degree ≤1〞,simulated magnitude≥5 that meet calibration requirements of the current high-precision optical navigation sensor.


2001 ◽  
Author(s):  
John V. Vallerga ◽  
Jason B. McPhate ◽  
Adrian P. Martin ◽  
Geoffrey A. Gaines ◽  
Oswald H. W. Siegmund ◽  
...  

2018 ◽  
Vol 45 (3) ◽  
pp. 315-350 ◽  
Author(s):  
M. Pavlinsky ◽  
A. Tkachenko ◽  
V. Levin ◽  
A. Krivchenko ◽  
A. Rotin ◽  
...  

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