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中国空间科学技术
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25 June 1998, Volume 18 Issue 03
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CHINA’S CDAS OF METEOROLOGICAL SATELLITE FY2
Tong Kai(Chinese Academy of Space Technology,Beijing 100081)
1998, 18 (
03
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Abstract
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1739
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The Command and Data Acquisition Station (CDAS) of the meteorological satellite FY2 is a first Chinese advanced comprehensive station.It integrates remote sensing image receiving and real time processing,broadcasting cloud pictures of different type,data communications,tracking,telemetry and command,trilateration ranging and satellite attitude determination.This paper describes its tasks.constructions and functions.The system block diagram and main specifications of the system and subsystems are given.The overall situation of design and development process are also analysed.
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DESIGN OF THE SYNCHRONIZERTIMER OF SYNCHRONIZER/DATA BUFFER SYSTEM
Gong Derong(Beijing Institute of Control Engineering,Beijing 100080)
1998, 18 (
03
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Abstract
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1724
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SynchronizerTimer is an important instrument of the Synchronizer/Data Buffer (S/DB) system for Command and Data Acquisition Station (CDAS).The device contains a highaccuracy digital phase locked loop that can precisely recover synchronizationbasic information from geostationary meteorological satellite cloud pictures.The Digital phase locked loop includes a phase comparator made up of high speed elements and a filter implemented by computer software.It applies standard frequency count mode and can complete the tracking of analog sun(highprecision sun pulse)and digital sun (scan synchronization digital),and measures the clock frequency on satellite,etc.At the same the microcomputer can server as a system manager.
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VISIBLE AND INFRA RED SPIN SCANNING RADIOMETER DATA PROCESSING METHOD
Fan Shiming Liu Jian Qian Liqun Zhong Fang (Beijing Institute of Satellite Information Engineering,Beijing 100080)
1998, 18 (
03
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Abstract
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1558
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The method of VISSR data buffering and processing is the key topic to design and manufacturing VISSR data processing subsystem for CDAS of FY 2 geostationary meteorological satellite.It will affect the accuracy and quality of the stretched Vissr(S.V.).The principle and calculating method of the processing model in which the data are first buffered and then resampled are discussed in this thesis.The technical way that the VISSR data are equal angle resampled using high speed parallel processor consisting of multi DSP is also introduced.
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THE CDAS AUTOMATIC MONITORING AND CONTROLLING SYSTEM
Chen Xiaohua Wang Yanguang Li Jilin Huang Canlin(Beijing Institute of Satellite Information Engineering,Beijing 100080)
1998, 18 (
03
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Abstract
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1574
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Command and Data Acquisition Station (CDAS) monitoring and controlling system absorbed the advanced experience at home and abroad.The advanced technology of modern computer management was used synthetically.This paper introdues the system plan,system structure and application software design.
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A REALTIME TELEMETRY AND ATTITUDE DETERMINATION SYSTEM BASED ON MULTILEVEL FAULT-TOLERANT
Sun Baoxiang Li Mingtao Wang Dongsheng Gao Yijun Hua GengxinLiu Chengxi Wang Changlong Jian Ming Wang Yuanxi Bai Zhiying(Beijing Institute of Control Engineering,Beijing 100080)
1998, 18 (
03
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Abstract
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1570
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The CDAS realtime telemetry and attitude determination system of meteorological satellite FY2 is a system of multifunction long life time and high reliability ,based on multiprocessor concurrent processing and multilevel faulttolerant architecture.It implements integrally realtime processing of analog telemetry including demodulation of accurate sun pulse,realtime determination of satellite's attitude,coding telemetry demodulation and realtime data processing,satelliteground loop simulation test,and processing of mass data,graphics and characters,communication and recording in realtime,etc.
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TELEMETRY DECODING SYSTEM DESIGN OF FY2 CDAS
Wang Xi(Beijing Institute of Spacecraft System Engineering,Beijing 100086)
1998, 18 (
03
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Abstract
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1835
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The telemetry decoding system of FY2 CDAS is used to demodulate coded telemetry signal to get information from Chinese FY2 meteorological satellite.The operators then analyze all these decoded data in order to know the working status of the satellite in detail.These decoded data are also transmitted to the SOCC.A redundant design,including active part and backup,enhances the reliability of the system.In case of the active equipment is out of order,the running of backup can be automatically switched.In this paper,the designing methods for a reliable telemetry decoding system are given,including subcarrier demodulation,frame synchronization,IRIGB time decoding,real time data analysis on computer etc.
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DESIGN OF RANGING SYSTEM IN CDAS
Zhang Tingxin(Xi'an Institute of Space Radio Technology,Xi'an 710000)
1998, 18 (
03
): .
Abstract
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1555
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In order to accomplish the trigonomotric ranging of FY2 meteorological satellite,the ranging instrument has been developed.This paper introduces the functions and application of the ranging instrument,describes the principle of ranging with multi sidetone and measurement procedure,and also gives the characteristic and composition of the system.A pure sidetone ranging system was designed,and the specification and performance of this system was discussed.
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SYNCHRONIZATION TECHNIQUE FOR CLOUD IMAGE DATA
Yan Jiazhen(Xi'an Institute of Space Radio Technology,Xi'an 710000)
1998, 18 (
03
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Abstract
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1651
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The frame period of satellite image changes suddenly,A positioning aperture technique is implemented to reliably acquire the frame period.With the help of subframe protection technique,the actual system works continuously,stably and reliably.
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METEOROLOGICAL SATELLITE CDAS RAW IMAGE DEMODULATOR
Xu Xing(Xi'an Institute of Space Radio Technology,Xi'an 710000)
1998, 18 (
03
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Abstract
(
2007
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This paper presents a new methodfourth law loop switching method,which is based upon the traditional fourth law loop and is suitable for fast acquisition.According to this principle,we develop a FY2 meteorological satellite CDAS raw image demodulator which has the properties of easy designing and adjusting,fast acpuisition,wide capture range and good bit error rate performance.Both testing and actual use prove that this demodulator achieves good specifications and can fully satisfy the actual demands.
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INTERMEDIATE FREQUENCY TRACKING AND TELEMETRY RECEIVER OF CDAS
Xi Qingling Li Genbao(Xi'an Institute of Space Radio Technology,Xi'an 710000)
1998, 18 (
03
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Abstract
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1726
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This paper introduced designing principles and realizing methods of tracking and telemetry receiver of CDAS of FY2 satellite.The receiver has short pullin time,large dynamic range,wide tracking range and small zero drift.By using switching control,the receiver can automatically follow the Japanese GMS satellite.Test results of the receiver are satisfied and superior to the specification.
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A TURNAROUND STATION IN TRILATERATION RANGING SYSTEM
Lan Maotian(Xi'an Institute of Space Radio Technology,Xi'an 710000)
1998, 18 (
03
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Abstract
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1524
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The Ulumqi and Guangzhou turnaround ranging stations developed by the company of the author and the Beijing master station compose a threepoint ranging system.This system can perform the function of the ranging and orbit determination of FY2 satellite.This article mainly introduces the configuration,function and technical specification of the turnaround ranging stations.Compared to the same type of the products abroad,this type of station has some distinguished features and has passed the design review of all levels. The stations were used in the tracking of the Japanese Meteorological satellite.The design of the turn around ranging station has been proved to be feasible and reasonable by the successful ranging and orbit determination of the FY2 satellite.
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METHOD OF CORRECTING DOWN LINE FREQUENCY SHIFT AND CALCULATING POINT FREQUENCY
Jiang Zhensheng(Beijing Institute of Satellite Information Engineering,Beijing 100080)
1998, 18 (
03
): .
Abstract
(
1581
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During FY2 satellite operating in orbit ,the local oscillator will have some frequency shift.It limits the frequency capture range of Data Collection Platform Receiving system(DCPR) corresponding to phase-locked loop of Data Collection Platform (DCP) information. In some serious eases the meteorological data collected by DCP can't be demodulated,so the system can't run normally. In order to resolve the above-mentioned problem, in this paper the method of down line frequency shift and calculating point frequency is discussed.The result of testing FY2 in orbit is satisfactory and shows that even if random interference is much serious, the succes probability of DCPR reception and modulation is over 98%.
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THE DESIGN OF CDAS 20m ANTENNA SUBSYSTEM
Song Linhui(The North West China Research Institute of Electronic Equipment,Xi'an 710065)
1998, 18 (
03
): .
Abstract
(
1804
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This paper introduces the configuration,characteristics and system design of the antenna subsystem,which meets relevant requirements of the Command and Data Acquisition Station (CADS) of FY2 China′s first geostationary meteorological satellite.CDAS antenna subsystem mainly consist of antenna mechanical Structure,feed network,antenna control unit (ACU) and monitoredcontrol (MAC).This antenna is a 20m modified cassegrain antenna,its feed is a corrugated horn,and adopts multiplemoulding autotrack monopulse method.The servo position loop consists of the angle encoder.Antenna is driven by 3phase SCR and servoDC motor.The backlash is eliminated by using dualmotor.ACU has multipleoperation modes and is easy controlled.ACU monitors working parameters and status of system,and detects the errors online.
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