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971.
    
Mechanisms of formation of cyclonic vortices in the tropical atmosphere of the Earth are investigated in the intratropical zone of convergence using numerical simulation made with the complete system of equations of gas dynamics taking into account transport of infrared radiation, phase transitions of water vapor into microdrops of water and ice particles, and sedimentation of these drops and ice particles in the field of gravity force. Observational data on the structure of dominant air streams, which are formed in the intratropical zone of convergence over the North Atlantic in the periods of its highest thermodynamic intensity and instability, are used in the initial and boundary conditions of the model. Formation of cyclonic vortex flows is obtained numerically at sufficiently strong bending of the intratropical zone of convergence. The results of numerical modeling are compared with the data of satellite microwave monitoring: global radio thermal fields of the Earth from the electronic collection GLOBAL-Field allowing one to study the structure of atmospheric motions in a wide range of space-time scales.  相似文献   
972.
The plasma Environment of Mars   总被引:1,自引:0,他引:1  
Nagy  A.F.  Winterhalter  D.  Sauer  K.  Cravens  T.E.  Brecht  S.  Mazelle  C.  Crider  D.  Kallio  E.  Zakharov  A.  Dubinin  E.  Verigin  M.  Kotova  G.  Axford  W.I.  Bertucci  C.  Trotignon  J.G. 《Space Science Reviews》2004,111(1-2):33-114
Space Science Reviews -  相似文献   
973.
The Ultraviolet Coronagraph Spectrometer (UVCS) on the Solar and Heliospheric Observatory (SOHO) has been used to measure spectral line profiles for H I Lyα in the south polar coronal hole at projected heliocentric heights from 3.5 to 6.0 R during 1998 January 5–11. Observations from 1.5 to 2.5 R were made for comparison. The H I Lyα profile is the only one observable with UVCS above 3.5 R in coronal holes. Within this region the outflowing coronal plasma becomes nearly collisionless and the ionization balance is believed to become frozen. In this paper, the 1/e half widths of the coronal velocity distributions are provided for the observed heights. The velocity distributions include all motions contributing to the velocities along the line of sight (LOS). The observations have been corrected for instrumental effects and interplanetary H I Lyα. The half widths were found to increase with projected heliographic height from 1.5 to 2.5 R and decrease with height from 3.5 to 5 R. This revised version was published online in June 2006 with corrections to the Cover Date.  相似文献   
974.
    
On February 4, 1986 Halley passed through inferior conjunction with Venus but was at high latitudes. Not all data for this time period have been received. However, the data that are available suggest that at most only weak effects associated with Halley were seen at Pioneer Venus. The data during this time, however, are useful for correlating with the behavior of the plasma tail.  相似文献   
975.
Teodosiev  D.  Stanev  G.  Galev  G.  Neichev  S.  Pushchaev  P. 《Cosmic Research》2000,38(6):574-578
The reliability and precision of satellite measurements of electric fields are significantly determined by the performance of probes used for these purposes. For measurements of the vector of the constant electric field and three components of the variable electric field in the frequency band from 0.1 Hz to 20 kHz on the INTERBALL-2 satellite, the method of a double probe and the scheme of three pairs of sensors are used. In manufacturing the sensitive units of the probes, an original Bulgarian technology for glass-carbon coating on their spherical surfaces was used. The results of measurements (by the Siesmann–Kelvin method) of variations of electron work function from the surface of the spherical probes with glass-carbon coating have shown mean statistical variations W < 0.006 eV. To minimize the errors in measuring electric fields, a construction of the probes as monoblocks with balancing and guarding electrodes was developed and used. The guarding electrodes are under a bias voltage in the limits from 0 to 12 V to decrease the influence of currents caused by photoelectrons emitted by different units of the satellite construction. The value of this bias was determined by choosing the working point of the voltage–current characteristic. The optimum value of the bias current for the auroral area was in the limits 70–100 nA. Output signals from the sensors of the IESP-2M instrument were used in measuring electric fields by the MEMO and NVK-ONCh instruments included in the wave complex.  相似文献   
976.
    
A familiar two-transistor saturable-core parallel inverter is modeled as a nonlinear negative resistance in parallel with energy-storage elements. The techniques of singular-point analysis are combined with piecewise linear techniques to permit determination of solution trajectories on the phase plane. Clear insight is provided, not only into steady-state oscillation, but also into transient behavior of the circuit. Experimental results confirming the analytical model are included.  相似文献   
977.
    
This work is a continuation of the previous article and it focuses on low solar activity and modeling effort. NeQuick model uses Epstein layer formalism to model each part of the profile. We study the diurnal and seasonal variations of B2bot, ΔB2 (B2best − B2NeQuick2) and R (B2best/B2NeQuick 2) at Hainan station during low solar activity. The results show it is possible to improve the B2bot parameter of the NeQuick model at that region during low solar activity. Then, we use a function ?(t) with LT in different seasons to correct the B2bot formula of NeQuick 2. The correction shows that (1) By the correction formula, the B2bot of NeQuick is improved. The maximum standard deviation is improved for 9 km. (2) The correction formula is more effective in summer than in equinox and winter and performs better during early morning hours than during the rest of the day.  相似文献   
978.
    
Satellite gravity field missions such as CHAMP, GRACE and GOCE are designed as low Earth orbiting spacecraft (LEO) with orbit heights of about 250–500 km. The challenging mission objectives require a very precise knowledge of the satellite orbit position in space. For these missions precise orbit information is typically provided by GPS satellite-to-satellite tracking (SST) observations supported by satellite laser ranging (SLR).  相似文献   
979.
980.
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