卫星控制系统测试数据自动判读系统设计

Abstract

Abstract: Considering the mass data and complex types of test data for satellite control system, the artificial diagnostic method has many shortages such as the long interpreting time and inadequate of diagnostic precision. The test data are analyzed according to their transforming rules, and the diagnostic rule of test data is established. A new method is offered to automatically diagnose test data, and the corresponding design is given for control system based on those models． This system not only diagnoses data via the configured rules, but also records diagnostic results. Thus this system improves the test efficiency and the diagnostic veracity.

Key words: control system, test data, automatic diagnosis, diagnostic rule

CLC Number:

V557

WU Jing, LU Wen-Gao, CHANG Wu-Jun. Design of Automatically Diagnostic System of Test Data for Satellite Control System[J]., 2014, 40(6): 53-57.

References

［1］党建成，俞洁，周晶．FY2卫星综合测试系统自动测试技术［J］．上海航天，2005(1)：7277. DANG J C, YU J, ZHOU J. Automatic measurement technology of integrated test system for FY2 meteorological satellite ［J］. Aerospace Shanghai, 2005(1):7277. ［2］吴限德，孙兆伟，陈卫东．小卫星测试数据在线时间序列判读方法［J］．哈尔滨工程大学学报，2012,33(3)：383388. WU X D, SUN Z W, CHEN W D. An online data interpretation method in a microsatellite ground test system based on a time series analysis［J］. Journal of Harbin Engineering University, 2012,33(3):383388. ［3］吴晓，赵光恒，于英杰,等．仿真测试自动判读专家系统的设计与实现［J］．系统仿真学报，2005，17(12)：30503052． WU X, ZHAO G H, YU Y J, et al. Designing and realizing automatically diagnostic expert system for simulation test［J］. Journal of System Simulation, 2005,17(12):30503052. ［4］赵峰，文博武，孙洁,等．基于卫星数据判读的一种方法［C］//第十六届全国测试与故障诊断技术研讨会论文集. 北京：中国计算机自动测量与控制技术协会，2007：225229. ZHAO F, WEN B, SUN J, et al. An interpretation method based on satellite data［C］//The 16th National Testing and Fault Diagnosis Technology Conference. Beijing: China Computer Automated Measurement and Control Technology Association, 2007:225229. ［5］李砥擎，朱维宝，王庆成，等．一种用于航天器数据监视的知识表示方法［J］．计算机测量与控制，2006,14(3)：289292. LI D Q, ZHU W B, WANG Q C, et al. Knowledge representation approach to spacecraft data monitoring［J］.Computer Measurement & Control, 2006,14(3):289292. ［6］曹永梅，周剑敏，潘立鑫．卫星控制系统测试数据自动判读系统的设计与实现［J］．空间控制技术与应用，2013，39(5)：5862． CAO Y M, ZHOU J M, PAN L X. Design and implementation of automatic data discrimination system for satellite control system［J］. Aerospace Control and Application, 2013, 39(5):5862. ［7］谢明明，沈湘衡，贺庚贤,等．空间相机仿真测试数据自动判读系统的设计［J］．计算机测量与控制，2010,18(6)：12771279. XIE M M, SHEN X H, HE G X, et al. Design of data automatically diagnostic system for simulation test with space camera［J］. Computer Measurement & Control, 2010,18(6):12771279. ［8］戴居峰，袁利，王跃．基于开放式结构的航天器控制系统测试技术研究［J］．空间控制技术与应用，2012，38(5)：3437． DAI J F, YUAN L, WANG Y. OSAbased testing technology of spacecraft control system［J］. Aerospace Control and Application, 2012, 38(5):3437. ［9］秦巍，郭永富．一种基于历史遥测数据的在轨卫星故障预警系统［J］．航天器工程，2010,19(6)：4045. QIN W, GUO Y F. A failure warning system based on historical telemetry data for satellites on orbit［J］. Spacecraft Engineering, 2010,19(6)：4045.

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Design of Automatically Diagnostic System of Test Data for Satellite Control System

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