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141.
Secondary radioactive isotopes that are used for the determination of cosmic-ray age have relatively short decay lifetimes.
The measured abundance of these isotopes at low energies is representative of the cosmic-ray diffusion and the gas distribution
in a region of a few hundred parsecs around the Sun. We show how to determine the local cosmic-ray diffusion coefficient in
the Galaxy using the data on decaying cosmic-ray nuclei. Calculated surviving fractions of decaying secondary isotopes in
diffusion and leaky box models are presented.
This revised version was published online in June 2006 with corrections to the Cover Date. 相似文献
142.
A. I. Eriksson R. Boström R. Gill L. Åhlén S.-E. Jansson J.-E. Wahlund M. André A. Mälkki J. A. Holtet B. Lybekk A. Pedersen L. G. Blomberg 《Space Science Reviews》2007,128(1-4):729-744
The Rosetta dual Langmuir probe instrument, LAP, utilizes the multiple powers of a pair of spherical Langmuir probes for measurements
of basic plasma parameters with the aim of providing detailed knowledge of the outgassing, ionization, and subsequent plasma
processes around the Rosetta target comet. The fundamental plasma properties to be studied are the plasma density, the electron
temperature, and the plasma flow velocity. However, study of electric fields up to 8 kHz, plasma density fluctuations, spacecraft
potential, integrated UV flux, and dust impacts is also possible. LAP is fully integrated in the Rosetta Plasma Consortium
(RPC), the instruments of which together provide a comprehensive characterization of the cometary plasma.
The LAP Team is listed in Table III. 相似文献
143.
Sources of Ion Outflow in the High Latitude Ionosphere 总被引:4,自引:0,他引:4
Ion composition observations from polar-orbiting satellites in the past three decades have revealed and confirmed the occurrence of a variety of ion outflow processes in the high-latitude ionosphere. These processes constitute a dominant source of ionospheric plasma to the Earth's magnetosphere. We review the current state of our observational knowledge on their occurrence, energy, composition, variability, interrelationships, and quantitative contributions to the overall mass input to the magnetosphere. In addition, we identify the prevalent sources and the gaps of our current understanding of these sources. 相似文献
144.
P. S. Thé L. Matveyenko J. Kleczek L. M. Gindilis G. M. Rudnitskij J. Arbocz J. Schuve J. A. Steketee W. de Graaff K. A. van der Hucht Wayne G. Roberge G. Kockarts R. H. van Gent E. Dekker T. S. van Albada D. de Hoop H. Nieuwenhuijzen Josip Kleczek J. L. van Ingen P. Hellings A. Achterberg 《Space Science Reviews》1985,41(1-2):201-213
145.
Kleczek J. van Gent R. H. Rutten Robert J. de Munck J. C. Slottje C. Severne G. Pecker Jean-Claude Postma H. Grishchuk L. P. Niewenhuijzen H. Schuiling R. D. van Beek H. F. Reijnen G. C. M. Heidmann Jean Lemaire J. Bleeker Johan Icke V. Neéman Y. Feast M. W. de Graaff W. 《Space Science Reviews》1986,43(3-4):383-396
Space Science Reviews - 相似文献
146.
B. Van der Holst S. Poedts E. Chané C. Jacobs G. Dubey D. Kimpe 《Space Science Reviews》2005,121(1-4):91-104
Simulations of coronal mass ejections (CMEs) evolving in the interplanetary (IP) space from the Sun up to 1 AU are performed
in the framework of ideal magnetohydrodynamics (MHD) by the means of a finite-volume, explicit solver. The aim is to quantify
the effect of the background solar wind and of the CME initiation parameters, such as the initial magnetic polarity, on the
evolution and on the geo-effectiveness of CMEs. First, three different solar wind models are reconstructed using the same
numerical grid and the same numerical scheme. Then, different CME initiation models are considered: Magnetic foot point shearing
and magnetic flux emergence. For the fast CME evolution studies, a very simple CME model is considered: A high-density and
high-pressure magnetized plasma blob is superposed on a background steady state solar wind model with an initial velocity
and launch direction. The simulations show that the initial magnetic polarity substantially affects the IP evolution of the
CMEs influencing the propagation velocity, the shape, the trajectory (and thus, the geo-effectiveness). 相似文献
147.
148.
149.
In safety-critical systems such as transportation aircraft, redundancy of actuators is introduced to improve fault tolerance. How to make the best use of remaining actuators to allow the system to continue achieving a desired operation in the presence of some actuators failures is the main subject of this paper. Considering that many dynamical systems, including flight dynamics of a transportation aircraft, can be expressed as an input affine nonlinear system, a new state representation is adopted here where the output dynamics are related with virtual inputs associated with the intended operation. This representation, as well as the distribution matrix associated with the effectiveness of the remaining operational actuators, allows us to define different levels of fault tolerant governability with respect to actuators’ failures. Then, a two-stage control approach is developed, leading first to the inversion of the output dynamics to get nominal values for the virtual inputs and then to the solution of a linear quadratic(LQ) problem to compute the solicitation of each operational actuator. The proposed approach is applied to the control of a transportation aircraft which performs a stabilized roll maneuver while a partial failure appears. Two fault scenarios are considered and the resulting performance of the proposed approach is displayed and discussed. 相似文献
150.
Bozdağ Ebru Ruan Youyi Metthez Nathan Khan Amir Leng Kuangdai van Driel Martin Wieczorek Mark Rivoldini Attilio Larmat Carène S. Giardini Domenico Tromp Jeroen Lognonné Philippe Banerdt Bruce W. 《Space Science Reviews》2017,211(1-4):571-594
Space Science Reviews - We present global and regional synthetic seismograms computed for 1D and 3D Mars models based on the spectral-element method. For global simulations, we implemented a... 相似文献