2005 Vol. 25, No. 4

Display Method:
Numerical Simulation of CME Initiation and Propagation From a Streamer Containing Nested Close Magnetic Field Structures
YEI Zhanyin, WEI Fengsi, WANG Chi, FENG Xueshang, ZHONG Dingkun
2005, 25(4): 241-247. doi: 10.11728/cjss2005.04.20050401
Abstract(2478) PDF 2182KB(1151)
Abstract:
Qualitative numerical result of a special type of Coronal Mass Ejection (CME) is presented. The magnetic field direction in front half part of central closed magnetic field of the CME is opposite to that of the solar global dipole. Numerical result shows that:between the two anti-directional magnetic field lines of the CME magnetic field and the solar global dipole, there exists a transitional magnetic field structure, the area scale of which becomes gradually large when CME propagates outward. The numerical result may explain why spacecrafts can observe a type of bipolar magnetic cloud, in front half of which, the magnetic field direction is opposite to that of the solar global dipole. To obtain the numerical result, a background streamer with nested close magnetic field lines in it plays a central role for the CME initiation and propagation. The background steady state solution is approached by a long time interaction between a potential magnetic field and Parker solar wind solution. The potential magnetic field is obtained by properly combining a dipole and a hexapole. Because for the dipole, interaction between the potential magnetic field and solar wind can not open the dipole up and a streamer containing nested close magnetic field structures for triggering the CME at a suitable position forms finally.
Excited Low Frequency Waves by Beam Plasma in Upstream of Collisionless Shock and Their Effect on Dissipation of Shock
GUO Fan, LU Quanming, WANG Shui
2005, 25(4): 248-253. doi: 10.11728/cjss2005.04.20050402
Abstract(2711) PDF 1755KB(1152)
Abstract:
Due to the reflection by collisonless shock, ion beam can be formed in upstream of collisionless shock. In this paper, a one-dimensional hybrid simulation is performed to investigate beam plasma instabilities for two cases:low (nb/n0=0.02) and high (nb/n0=0.2) beam densities, where nb and n0 represents the beam and background plasma density respectively. The results show that for low beam density the beam mainly excites the right-polarized waves through resonance interaction. The waves propagate parallel to the ambient magnetic field, and they can only decelerate a.nd heat the beam protons. When the beam density is high, the beam can excite the waves with propagation direction parallel and anti-parallel to the ambient magnetic field. These waves can interact with beam protons relying on resonance condition, while they interact with background protons due to non-resonant effects. Besides decelerating and heating the beam protons, they can also accelerate and heat the background protons. Their effects on the dissipation of quasi-parallel collisionless shock are also discussed.
Ionospheric Disturbances Produced by Artificially Chemical Releases
HUANG Wengeng, GU Shifen
2005, 25(4): 254-258. doi: 10.11728/cjss2005.04.20050403
Abstract(2616) PDF 1263KB(1300)
Abstract:
Active experiments in the ionosphere, which give rise to artificial disturbances of electron density, are usually conducted by the injection of chemical clouds at ionospheric altitudes. Their effect has often been called an ionospheric hole simply to dramatize the localized nature of the disturbances, which had been observed in many experiments. For example, the injection of rocket exhaust neutral molecules into ionosphere, predominantly H2O and H2, can result in ionospheric electron density depletion. Main physical mechanism in these experiments is due to ion and molecule exchange reactions, which enhance the effective rate of recombination of electron. Ionospheric disturbances produced by artificially chemical releases have many applications in radio propagation and exploring ionosphere and plasma physics study. In terms of diffusion process of neutral gas and relevant chemical reactions in terrestrial ionosphere, the theoretical model of ionospheric modification created by active chemical releases is investigated in this paper. The influences of injected H2O and SF6 gas on the ionosphere under exponential atmosphere background are theoretically calculated, respectively. The results show that diffusion process of the injected neutral gas at ionospheric height is very quick, and the two released chemical materials can produce localized electron density depletions in F-regions, and those released materials, which have slow diffusion speed and large chemical reaction rates, will substantially affect ionosphere, and facilitate formation of artificial ionospheric hole.
Analysis of the Intense Magneticstorm of July, 2000 and of October, 2003 Using the Technique for Nowcasting of GPS TEC Data
XIA Chunliang, WAN Weixing, YUAN Hong, ZHAO Biqiang, DING Feng
2005, 25(4): 259-266. doi: 10.11728/cjss2005.04.20050404
Abstract(2383) PDF 2387KB(1133)
Abstract:
With a worldwide GPS network, the data of the July 14-18, 2000 geomagnetic storm and the October 28-November 1, 2003 storm is studied and compared using the technique for nowcasting of GPS TEC developed by the ionospheric station of Wuhan ionosphere observatory. In this paper, the ionospheric responses and the TEC variation during these two storms are discussed, especially the reducing and moving of the perturbation structure around the geomagnetic equator during storms and the ionospheric responses of high latitude part are analyzed. The results show that the ionospheric responses during these two storms are different and this difference is primarily caused by the seasonal difference of the magnetospheric energy deposition into the polar upper atmosphere. It is shown that the TEC variation is associated with the local time the solar perturbing occurred and the coupling of the ionospheric particles of high latitude with the solar particle. If there are several magnetic storms occurring in series, the ionospheric responses are more complex and disordered than the state that only one storm occur in a few days.
Observations of the Mesospheric and Lower Thermospheric Mean Winds at 30°N With MF radars
ZHANG Dongya, HU Xiong, ZHANG Xunxie, WU Xiaocheng, K. Igarashi
2005, 25(4): 267-272. doi: 10.11728/cjss2005.04.20050405
Abstract:
Winds data of Wuhan (30.5°N, 114.4°W) MF radar available during 2001-01-01-03-18, 2002-02-05-03-18, and 2002-10-18-12-31, Yamagawa (31.2°N, 130.6°W) MF radar of Japan available during 1997-01-01-10-17 were used to analyze features of the mesospheric and lower ther-mospheric mean winds within 60-98km altitude ranges at near 30°N. It is shown that there are obviously seasonal variations in mean zonal winds and mean meridional winds. Westerly winds prevail in winter mean zonal winds, and decrease versus increasing heights, and even reverse near the top sometimes. During summer, Easterly winds prevail in the mesosphere but westerly winds prevail in the lower thermosphere. The summer zonal wind reversed height is about 80km. The spring and autumn are the transition time between summer structures and winter structures. An easterly winds tongue shows in spring. In the mesopause regions near 80km the mean meridional winds blow northwards during winter time, but southwards during summer time. Mean winds also show inter-annual variability. The above climate features of mean winds agree very well with the HWM93 model.
The Progress of Chinese Space Medicine
YUAN Ming, JIANG Shizhong
2005, 25(4): 273-279. doi: 10.11728/cjss2005.04.20050406
Abstract(2966) PDF 2965KB(1380)
Abstract:
Space medicine is a new special medicine which is rising with the development of manned space program and has acquired great development during the space exploitation since established. In the early of 1990s, manned space flight program was initiated in china. However, the history of development for Chinese space medicine commenced in 1950s. Especially during the past ten years, the initiation of Chinese manned space flight program has brought great opportunity to Chinese space medicine. Presently, the first manned space flight has acquired consummation in china. Space medical specialists have experienced the trial of the first manned space flight as well as the first Chinese astronaut who has landed safely and healthily. During the past 40 years, the area of research in Chinese space medicine has gradually expanded, including the subjects such as gravitational physiology, cell and molecular biology, space environmental medicine, space psycology and space implemental medicine et al. The studies in Chinese space medicine are developing steadily. In the following Chinese manned space program, many difficulties will be more complex and need to be resolved for the success of spaceflight program. At the same time, this is also a challenge to the Chinese scientist. The article will briefly introduce the basic and applicational research of Chinese space medicine including their progress and give the outlook of their challenge and opportunity in the future.
The Analysis and Simulation of Co-Frequency Interference in Non-Geostationary Orbit Satellite Network
LI Rui, ZHAO Hongli, ZENG Dexian
2005, 25(4): 280-285. doi: 10.11728/cjss2005.04.20050407
Abstract(2539) PDF 1768KB(1270)
Abstract:
With the increasing of non-geostationary orbit satellite systems, the frequency bands allocated to the non-geostationary orbit satellite are getting less, which would bring the co-frequency interference for data transmission in down-link of non-geostationary orbit satellite network. The ratio C/I between the useful received carrier power and the overall contribution at the receiver input of interference power can show the interference situation. This ratio depends on the system characteristics, such as type of orbits, number of satellites in the constellation, antenna radiation patterns, etc. This paper analyses the problem of co-frequency interference, according to the time-varied character of non-geostationary orbit satellite the paper introduces a method to calculate co-frequency interference. The co-frequency interference is simulated and the results is analyzed, then, visualization of the interfering course is realized which can dynamically display the changes of interference-link during the different simulation periods.
A New Autonomous Celestial Navigation Method for Deep Space Probe and Its Observability Analysis
NING Xiaolin, FANG Jiancheng
2005, 25(4): 286-292. doi: 10.11728/cjss2005.04.20050408
Abstract(2575) PDF 2103KB(1192)
Abstract:
Celestial navigation method is a kind of important autonomous navigation method for deep space probing. Now it is widely used in many situations, especially in deep space exploration for its special characteristics. There are two kinds of celestial navigation methods. One is to use the geometric technique, in which the navigation information is obtained from the geometric relation between the celestial bodies and explorer. The other is an optimal estimate technique, which uses the celestial measurement as observation directly and employs the extended Kalman filter to estimate the position of explorer. A new autonomous celestial navigation for lunar explorer is developed and investigated in this paper, which combines both these two techniques. At first using the geometric technique to calculate the position of satellite and then reestimate the original position determination results using orbit dynamical equations and Multiple Model (MM) Kalman filter to get a better navigation result. The simulation result shows the high precision of this new method. Finally, the superiority and effectiveness based on the observability and the degree of observability analysis of this method are demonstrated by the simulation result simultaneously.
Orbit Determination of Satellite on the Middle-High Earth Orbit Based on GPS
LIU Haiying, WANG Huinan
2005, 25(4): 293-297. doi: 10.11728/cjss2005.04.20050409
Abstract(2441) PDF 1433KB(1629)
Abstract:
The using of GPS (Global Positioning System) in space orbit solution is dicussed, especially in the application of HEO (Highly Eccentric Orbit) and GEO (Geodetic Earth Orbit). Aiming at the disadvantage factors of the shortage of visible emitter and weak GPS signal in the HEO and GEO, an efficient algorithm is developed for the acquisition of weak GPS C/A signals. The signals with very low signal-to-noise ratios can be successfully acquired. The capture ability of GPS receive is greatly enhanced that can capture the signal with SNR of 25 dB using the method introduced in this paper. At the same time an original technique based on pseudo-acceleration measurement to compute the fix solution with the spaceborne receiver is presented. The pseudo-acceleration measurements can be computed by pseudorange difference, and the relation between the position and the acceleration can be obtained by Newton's law. When only two transmitters are visible in HEO or only one transmitters is visible in GEO, the state of the receiver (position, velocity, clock bias, and drift) can be obtained. A simulation illustrates that the error is within 100 m in the orbit of 4000 km high and within 2 km in the height of 36 000 km. The simulation result shows that the method in this paper is effective.
Design of Orbit Debris Environment and Collision Alert System
MA Zhihao, CHEN Lei, ZHOU Bozhao
2005, 25(4): 298-303. doi: 10.11728/cjss2005.04.20050410
Abstract(2544) PDF 1766KB(1444)
Abstract:
Since the number of targets near the earth orbit has already been beyond 9000, it is necessary and much important to analyze targets near the mission orbit to bring the mission to access both before the launch and during the orbital mission. NORAD maintains general element perturbation element sets (Two-Line Element Sets, TLEs) on all resident space objects. In turn, these element sets are provided to users. These element sets are periodically refined so as to maintain a reasonable prediction capability on all space objects. At the same time, NORAD developed a set of models named SGP/SDP series as models for propagation of NORAD element sets. Five mathematical models for prediction of satellite position and velocity are available. And the NORAD element sets are currently generated with either SGP4 or SDP4 depending on whether the satellite is near-Earth or deep-space. These two models, SGP4 for "near-earth" objects and SDP4 for "deep space" objects, are widely used in satellite tracking software and can produce very accurate results when used with current NORAD two-line element datum. A brief review is taken at these element sets and propagation models first. Then through the precision analysis, it is believed that using SGP4/SDP4 models for taking quick collision alert among space targets is suitable. Based on this conclusion, an orbit debris environment and collision alert system was designed. In this system, targets and the corresponding TLEs are saved in a database based on MS SQL Server, and the data visual is realized by OpenGL. The orbit propagation models being used is SGP4/SDP4 since this model is the generator of current TLEs and will be supported in the future.
An Algorithm for the Orbital Evolution of Space Debris from Breakup Events
GONG Songbo, XU Minqiang, CUI Pingyuan, LI Shuang
2005, 25(4): 304-308. doi: 10.11728/cjss2005.04.20050411
Abstract(2136) PDF 1393KB(1379)
Abstract:
Space debris created by man's space activities has brought great risks to launch and operation of spacecrafts, especially in the following few years, there will be more and more space activities in the world. So it is necessary to know situation of current space debris environment and predict its development in the future, thus to provide important reference to protection design and operation of spacecrafts and measures of diminishing amount of space debris. An important component of the debris population that is presented in this paper is the debris generated by on-orbit breakup events. It is collision and explosion event that inflames most the increasing rate of the total amount of the space debris. Breakup events include collision and explosion events. Consequently the ability to model different breakup events is a vital part of a long-term debris environment model. In this paper, the orbital evolution of space debris from the spacecraft breakups has been done a through mathematical analysis. A detailed research on the mechanisms of space debris generation, evolution and annihilation from the view point of evolutionary mode is also given. The velocity increments of space debris from spacecraft breakups are presented. Based on the velocity increments, the orbital elements of space debris are gained. Then the cumulative number and orbital distribution of space debris are analyzed due to atmospheric drag perturbation. Finally, the relevant results are gave and compared with the results of CODRM. The results indicate the feasibility of the algorithm.
The Implementation and Verification of RS(255, 223) Decoder According to CCSDS Specification
SHI Junfeng, WANG Yu, SUN Huixian
2005, 25(4): 309-314. doi: 10.11728/cjss2005.04.20050412
Abstract(3591) PDF 1627KB(1312)
Abstract:
A RS (Reed-Solomon) code is an excellent linear cyclic block code in the error control field. It has found widespread use in deep space exploration and has been adopted by the spatial organizations such as CCSDS, NASA, ESA for its powerful random and burst error correcting ability. The research project adopts a new reformulated inversionless BM (Berlekamp-Massey) algorithm to fulfill a RS(255, 223) decoder according to CCSDS specification. In this paper, the algorithm, verification method and the verification platform based on PCI bus interface of the RS(255, 223) decoder have been introduced. The experiment result and the comparison of the theoretic and testing error probability of the decoder have been mentioned. The test result proves the complexity of the proposed decoder is only about 180 000 gates and has a throughput of 400 Mbps using FPGA. The error correcting ability of the decoder is normal.
Software Frame Synchronizer and Related Technology Research of Moving Window Display for CCD Data of CBERS-2
CAO Yu, YANG Renzhong
2005, 25(4): 315-320. doi: 10.11728/cjss2005.04.20050413
Abstract(2666) PDF 1773KB(1086)
Abstract:
The processing speed is the key problem of software frame synchronization. This article, using the arithmetic of KMP and Rabin-Karp, give an effective method in software frame synchronization, which increase the processing speed. And a software frame synchronizer was built and related test and analysis were made, the result was given in the paper. With the analysis of the data format of CBERS-2 (China-Brazil Earth Resources Satellite) and using the software frame synchronizer and the technology of DirectX display, a software moving window display system of the CBERS CCD two channels sensor was made. The effect of the overlap data of this satellite was lighten by some method. The software frame synchronizer and moving window display system can act as very important parts in a data recording system.