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There are many geometric calibration methods for “standard” cameras. These methods, however, cannot be used for the calibration of telescopes with large focal lengths and complex off-axis optics. Moreover, specialized calibration methods for the telescopes are scarce in literature. We describe the calibration method that we developed for the Colour and Stereo Surface Imaging System (CaSSIS) telescope, on board of the ExoMars Trace Gas Orbiter (TGO). Although our method is described in the context of CaSSIS, with camera-specific experiments, it is general and can be applied to other telescopes. We further encourage re-use of the proposed method by making our calibration code and data available on-line.  相似文献   
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An attempt to employ a magnetically driven shock tube as a tool for aerodynamic studies of high velocity and high enthalpy flows is described. Examples of results are given.  相似文献   
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Panning  Mark P.  Lognonné  Philippe  Bruce Banerdt  W.  Garcia  Raphaël  Golombek  Matthew  Kedar  Sharon  Knapmeyer-Endrun  Brigitte  Mocquet  Antoine  Teanby  Nick A.  Tromp  Jeroen  Weber  Renee  Beucler  Eric  Blanchette-Guertin  Jean-Francois  Bozdağ  Ebru  Drilleau  Mélanie  Gudkova  Tamara  Hempel  Stefanie  Khan  Amir  Lekić  Vedran  Murdoch  Naomi  Plesa  Ana-Catalina  Rivoldini  Atillio  Schmerr  Nicholas  Ruan  Youyi  Verhoeven  Olivier  Gao  Chao  Christensen  Ulrich  Clinton  John  Dehant  Veronique  Giardini  Domenico  Mimoun  David  Thomas Pike  W.  Smrekar  Sue  Wieczorek  Mark  Knapmeyer  Martin  Wookey  James 《Space Science Reviews》2017,211(1-4):611-650
Space Science Reviews - The InSight lander will deliver geophysical instruments to Mars in 2018, including seismometers installed directly on the surface (Seismic Experiment for Interior Structure,...  相似文献   
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Aymeric Spiga  Don Banfield  Nicholas A. Teanby  François Forget  Antoine Lucas  Balthasar Kenda  Jose Antonio Rodriguez Manfredi  Rudolf Widmer-Schnidrig  Naomi Murdoch  Mark T. Lemmon  Raphaël F. Garcia  Léo Martire  Özgür Karatekin  Sébastien Le Maistre  Bart Van Hove  Véronique Dehant  Philippe Lognonné  Nils Mueller  Ralph Lorenz  David Mimoun  Sébastien Rodriguez  Éric Beucler  Ingrid Daubar  Matthew P. Golombek  Tanguy Bertrand  Yasuhiro Nishikawa  Ehouarn Millour  Lucie Rolland  Quentin Brissaud  Taichi Kawamura  Antoine Mocquet  Roland Martin  John Clinton  Éléonore Stutzmann  Tilman Spohn  Suzanne Smrekar  William B. Banerdt 《Space Science Reviews》2018,214(7):109
In November 2018, for the first time a dedicated geophysical station, the InSight lander, will be deployed on the surface of Mars. Along with the two main geophysical packages, the Seismic Experiment for Interior Structure (SEIS) and the Heat-Flow and Physical Properties Package (HP3), the InSight lander holds a highly sensitive pressure sensor (PS) and the Temperature and Winds for InSight (TWINS) instrument, both of which (along with the InSight FluxGate (IFG) Magnetometer) form the Auxiliary Sensor Payload Suite (APSS). Associated with the RADiometer (RAD) instrument which will measure the surface brightness temperature, and the Instrument Deployment Camera (IDC) which will be used to quantify atmospheric opacity, this will make InSight capable to act as a meteorological station at the surface of Mars. While probing the internal structure of Mars is the primary scientific goal of the mission, atmospheric science remains a key science objective for InSight. InSight has the potential to provide a more continuous and higher-frequency record of pressure, air temperature and winds at the surface of Mars than previous in situ missions. In the paper, key results from multiscale meteorological modeling, from Global Climate Models to Large-Eddy Simulations, are described as a reference for future studies based on the InSight measurements during operations. We summarize the capabilities of InSight for atmospheric observations, from profiling during Entry, Descent and Landing to surface measurements (pressure, temperature, winds, angular momentum), and the plans for how InSight’s sensors will be used during operations, as well as possible synergies with orbital observations. In a dedicated section, we describe the seismic impact of atmospheric phenomena (from the point of view of both “noise” to be decorrelated from the seismic signal and “signal” to provide information on atmospheric processes). We discuss in this framework Planetary Boundary Layer turbulence, with a focus on convective vortices and dust devils, gravity waves (with idealized modeling), and large-scale circulations. Our paper also presents possible new, exploratory, studies with the InSight instrumentation: surface layer scaling and exploration of the Monin-Obukhov model, aeolian surface changes and saltation / lifing studies, and monitoring of secular pressure changes. The InSight mission will be instrumental in broadening the knowledge of the Martian atmosphere, with a unique set of measurements from the surface of Mars.  相似文献   
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基于虚拟现实的血管内介入手术三维导丝运动模拟   总被引:1,自引:0,他引:1  
导管和导丝在血管中的运动模拟在介入手术训练、计划及术中辅助治疗中具有重要意义。本文提出了一种快速有效的碰撞消除方法,开发了实时三维介入手术模拟系统,以模拟导管或导丝在实际血管中的运动行为。采用OpenGL图形库检测导管或导丝与血管壁之间的碰撞,通过几何分析和旋转角传播方法消除碰撞,最后对导管或导丝模型施加松弛过程,使其状态与实际状态更加吻合。实验结果表明,导管或导丝模型的运动状态与给定的材料参数密切相关,松弛过程使其状态更加自然,模拟可满足实时要求,方法可靠有效。  相似文献   
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