2002 Vol. 22, No. 2

Display Method:
FORCE-FREE MAGNETIC FIELDS WITH SINGULAR CURRENT DENSITY SURFACES AND THEIR STABILITY
HU Youqiu, LI Lin
2002, 22(2): 97-102. doi: 10.11728/cjss2002.02.20020201
Abstract(2190) PDF 486KB(1050)
Abstract:
Starting from the Bernstein's hydromagnetic energy principle, a general analysis is presented on the stability of a kind of one-dimensional force-free magnetic fields with singular current density surfaces and a single parameter in the cylindrical coordinates. The results obtained show that there exist stable and unstable regions in the parameter space. Their stability is determined solely by the radial distribution of the magnetic pitch in the neighborhood of the cylindrical axis, and irrelevant to the presence of the singular current density surface at the boundary.
PROPAGATION OF DISTURBANCES IN THE SOLAR CHROMOSPHERE-CORONA (Ⅱ)
LI Bo, ZHENG Huinan, WANG Shui
2002, 22(2): 103-112. doi: 10.11728/cjss2002.02.20020202
Abstract(1919) PDF 718KB(980)
Abstract:
In the first part of this article, the linear properties of MHD wave propagation is discussed. Then, in order to simulate the global characteristics of wave propagation in the solar chromosphere-corona, by employing a 2-dimensional time-dependent compressible MHD simulation subject to a self-consistent non-isothermal, non-uniform initial state, we study numerically the global propagation process of the disturbances initiated by a pressure pulse implemented at the bottom of chromosphere. Numerical results indicate that, in polar region, propagating disturbances can be distinguished into two modes, i.e. fast and slow magneto-acoustic waves. Whereas in the vicinity of solar equator, propagating disturbance is regarded as fast mode wave, and a standing disturbance is found to be located near the source region. These results may help explaining the wave events observed by SOHO/EIT.
ELECTROSTATIC PARTICLE SIMULATION OF SEE PHENOMENA IN IONOSPHERE
HUANG Wengeng, LE Guiming, GU Shifen
2002, 22(2): 113-118. doi: 10.11728/cjss2002.02.20020203
Abstract(2166) PDF 505KB(1124)
Abstract:
In this paper a particle-in-cell model is used to simulate the SEE (stimulated electromagnetic emission) produced by the parametric decay instability when a powerful high-frequency electromagnetic pump O-wave is launched into F-region of the ionosphere. The simulation results show the ratio of the pump wave frequency (w0) to the electron cyclotron harmonic frequency (wce) strongly influences the SEE when pump wave frequency is very close to the electron cyclotron frequency. Moreover the angle between the incident pump wave electric field and the geomagnetic field is also a considerable factor to the SEE. For example, for w0=4.2wce, the SEE is obvious, when the pump electric field is perpendicular to the geomagnetic field, but if the pump electric field is parallel to the geomagnetic field, there is no SEE phenomenon.
DERIVING EQUIVALENT WINDS FROM IONOSPHERIC F-LAYER DATA
LUAN Xiaoli, LIU Libo, LEI Jiuhou, WAN Weixing, NING Baiqi
2002, 22(2): 119-128. doi: 10.11728/cjss2002.02.20020204
Abstract(2202) PDF 906KB(870)
Abstract:
Deriving winds or electric fields from ionospheric data is very important for understanding thermospheric dynamics and ionospheric electrodynamics when the direct measurements are very limited. The methods previously used need a non-wind reference height, which is difficult to be accurately determined. In this paper, we develop a method to deduce the equivalent winds including effects of both neutral winds and electric fields from measured ionospheric F-layer data. The method avoids the problem of a non-wind reference height. Ionospheric data are available from the DGS-256 Digisonde in Wuhan to provide the critical frequency of F layer and its peak height with the aid of the new version SAO-Explorer software by University for Massachusetts Lowell in American. Using this method, some preliminary characteristics of equivalent winds in the ionospheric F layer over Wuhan are deduced during the summer and winter solstices, nine days ofvery quiet magnetic conditions in Winter of the year 2000-2001. The mean pattern of the vertical equivalent winds during the winter is also calculated.Resultsshow that there are clearly day-to-day variations of vertical equivalent winds over Wuhan. Obvious morning decent features are showed both in summer solstices and winter months. The difference from summer to winter solstice daytime vertical equivalent winds is discussed. In terms of the winter northward perpendicular drifts calculated from Fejer empirical electric fields, we find that the electric vertical drift generally contributes insignificantly to the vertical equivalent winds over Wuhan. Therefore, the mean equivalent winds are composed mainly from the meridional neutral winds.
AN IMPROVED GRID-BASED CORRECTION ALGORITHMS FOR THE IONOSPHERIC DELAY IN WAAS
WANG Yiju, YUAN Hong, WAN Weixing, ZHOU Jianhua, ZHU Mincai
2002, 22(2): 129-135. doi: 10.11728/cjss2002.02.20020205
Abstract(2354) PDF 903KB(1083)
Abstract:
Considering the Ionospheric TEC incline, We have given an improved Grid-based Correction Algorithm for ionospheric delay in Wide Area Augmentation System (WAAS). After computing with GPS data, we have got that the variance is 1/2 reduced compared with original Grid-based Correction Algorithm.
“SZ-2” ATMOSPHERIC DENSITY DETECTOR MEASUREMENT RESULT (I) CHANGE OF THE THERMOSPHERE DENSITY IN THE SUNSHINE AND SHADED AREA
QIN Guotai, QIU Shiyan, HE Aiqing, ZHU Yiqiang, SUN Lilin, LIN Xianwen, LI Hong, XU Xuepei
2002, 22(2): 136-141. doi: 10.11728/cjss2002.02.20020206
Abstract(2474) PDF 479KB(1027)
Abstract:
Solar radiation is the main source for heating of thermosphere. The change of its intensity can result in the change of Earth's upper atmospheric density. With the same reasons, the difference between the sunshine and shaded area is one of the main reasons for the difference of upper atmospheric density at the same altitude. For Low Earth Orbit (LEO) orbiter, when running around Earth, it will pass the sunshine area and shaded area each orbit even the orbit is circular or quasi-circular. Theconsequent change of atmospheric density directly influence orbiter's motions and the precision of prognostication of orbit. On the other hand, change of atmospheric density resulted from sunshining and shaded area has something to do with different factors of solar-terrestrial physics, some discussions are needed, takeing into about these related phenomena. Although data of American earlier balloon detection had already been applied to the discussion of diurnal-change of upper atmospheric density, due to limitation of the conditions at that time, detailed description of the change could not obtained. And the later AE, DE satellite etc. all run at elliptical orbits, could not provide data for the discussion of the phenomena above mentioned. In this article, we applied the data from "SZ-2" Atmospheric Density Detector, which are the direct measurement results at quasi-circular orbit and very helpful for the discussion of atmospheric density change in sunshine and shaded area. We separate the results and primary analysis into 2 parts: Characteristics of Change and Response to Solar and Geomagnetic Activity, and will describe them seperately. This paper is mainly concentrated on the first part. "SZ-2" Atmospheric Density Detector started orbitting around the earth on January 18, 2001. The orbital inclination was 41? and the flew altitude was 410 km. During the period of half a year, a lot of data of the upper atmospheric density have been obtained. In this paper, data of thermosphere density from February to April, 2001 collected by "SZ-2" Atmospheric Density Detector are used to study the change of the thermosphere density in the sunshining and shaded area. The results show that the ratio of the changes can be up to 2-3 in the vicinity of 410 km, and the magnitude of this change decreases as the geomagnetic activities increases. The peak value of the density in sunshining area increases as the solar activities increases and locates at the Local Time 14-15 h. The density in shaded area bear a relation to the geomagnetic activites, and increases as Ap value increases. The minimum value of the density in shaded area locates at the Local Time 4-5h. The latitude range of ?0?in the shaded area often show a density peak.
PLASMA PARAMETERS CONTROL WITH GRID IN A SIMULATED ENVIRONMENT OF LEO
PANG Yongjiang, XU Yuemin
2002, 22(2): 142-146. doi: 10.11728/cjss2002.02.20020207
Abstract(2210) PDF 391KB(1009)
Abstract:
The plasma generated by ECR plasma sources has a higher electron temperature and density. And the LEO plasma has lower ones. So we need to lower the temperature and density to simulate the LEO plasma environment in ground lab. By using a grid, grounded or with a bias volt, we successfully achieve the aim.
AUTONOMOUS CONTROL FOR SPACECRAFT
DAI Shuwu, SUN Huixian
2002, 22(2): 147-153. doi: 10.11728/cjss2002.02.20020208
Abstract(2248) PDF 655KB(1167)
Abstract:
A distributed multi-agents autonomous control system that satisfies the control needs of spacecraft is designed. The planning and scheduling subsystem that is composed of an abstract scheduling and a precise scheduling, is discussed in the paper. At last, a layered architecture is chosen for agent structure. Layered architecture allows integrating reactivity and deliberation together, which are all necessary for spacecraft control.
DYNAMICS OF DEPLOYMENT AND LIBRATION OF TETHERED SATELLITE SYSTEMS
GU Xiaoqin
2002, 22(2): 154-162. doi: 10.11728/cjss2002.02.20020209
Abstract(2308) PDF 602KB(1171)
Abstract:
The three-dimension dynamic equations of tethered satellite systems, with the mass of the tether considered, are formulated. The tension control rules and the optical relieving speed of the tether are derived by Pontryagin's method. A libra-tional motion of deployed system about the local vertical is studied. The movement couple between the center of mass and the attitude of tethered satellite systems is discussed, when the center of mass moves along Keplerian orbit. The numerical simulation results are included.
ATTITUDE AND RELATIVE POSITIONING ESTIMATION FOR FORMATION CONSTELLATION USING GPS
WANG Wei, XI Xiaoning, XU Qifeng
2002, 22(2): 163-168. doi: 10.11728/cjss2002.02.20020210
Abstract(2302) PDF 492KB(1120)
Abstract:
When determining attitude and relative position of formation constellation using carrier-phase differential GPS (CDGPS), the difference measurements of intra-satellite and inter-satellite must be combined to entirely resolve the states, because the states of the satellites are coupled and the difference measurements are correlative to each other. This paper presents a mathematical model of determining the attitudes and relative positions, which combining with intra-vehicle and inter-vehicle differential measurements, and using three-dimensional net constraint from inter-vehicle differential measurements. The mathematical simulation results show the feasibility of the method.
WASTEWATER TREATMENT AND MANAGEMENT IN SPACE STATION
ZHOU Kanghan, LI Junrong, LIU Chengliang, SHEN Liping
2002, 22(2): 169-176. doi: 10.11728/cjss2002.02.20020211
Abstract(2645) PDF 739KB(1231)
Abstract:
There need a mount of water in space station during long manned flight. To reduce the maintenance expanditure of flight, wastewater must be recovered and achieve a close loop circulation of water. The key task lies in resolving the problem of wastewater treatment and utilization and constituting a reasonable water circulation system based on the feature of wastewater in space station. In this paper, the wastewater treatment methods in space station are analyzed and compared, a space station integrated water management scheme was designed, and its rationality and feasibility are also discussed and verified from many aspects.
METAL HYDRIDE HEAT PUMP AND ITS APPLICATION IN THE LIFE SUPPORT SYSTEM OF MANNED SPACE FLIGHT
LIN Guiping, YU Minxian
2002, 22(2): 177-183. doi: 10.11728/cjss2002.02.20020212
Abstract(2233) PDF 682KB(1129)
Abstract:
In this paper, the working principle and research status of metal hydride heat pump are introduced, its application possibility to the life support system of manned space flight is analyzed. A comparison is made between different heat sinks, including water sublimator, phase change heat storage and metal hydride heat pump, from the aspects of size, weight, power, material waste and recovery time. The analysis shows that metal hydride heat pump system has wide application prospective in manned space flight. Some key techniques which must be considered firstly are stated.
EXPERIMENTAL STUDY ON PROTON IRRADIATION EFFECTS OF FLOATING GATE ROMS
HE Chaohui, GENG Bin, CHEN Xiaohua, YANG Hailiang
2002, 22(2): 184-192. doi: 10.11728/cjss2002.02.20020213
Abstract(2176) PDF 736KB(1063)
Abstract:
Experimental results of proton irradiation effects are given for Floating gate ROMs. The proton irradiation effects in FLASH ROM and EEPROM are the total dose effects rather than the Single Event Effects. These are attributed to the accumulative dose of both original and secondary protons. There is a proton fluence threshold. Errors occur when proton fluence is above the threshold. It is easy to eliminate the damage produced by proton irradiation for 29C256 by annealing in power on under 100癈, however, it is difficult for 28C256. Data errors occur in devices that are measured during irradiation and irradiated in power on, moreover, new data cannot be written in these devices with programmer. However, under more proton fluence, there is no error in devices in power off mode and new data can be written in these devices with programmer. It is an effective method to backup some devices in power off mode to improve the reliability of spacecrafts in which FLASH ROMs and EEPROMs are used.