Design and implementation of the highly-reliable, low-cost housekeeping system in the ZDPS-1A pico-satellite
计算机与自动化|Updated:2022-04-08
|
Design and implementation of the highly-reliable, low-cost housekeeping system in the ZDPS-1A pico-satellite
Design and implementation of the highly-reliable, low-cost housekeeping system in the ZDPS-1A pico-satellite
信息与电子工程前沿(英文)2012年13卷第2期 页码:83-89
Affiliations:
College of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310027, China
Author bio:
Yang-ming ZHENG, E-mail: zymsun2002@zju.edu.cn
Funds:
Project supported by the Foundation for the Author of National Excellent Doctoral Dissertation of China (No. 200035) and the Ministry of Education Science & Technology Research Project, China (No. 104069)
Design and implementation of the highly-reliable, low-cost housekeeping system in the ZDPS-1A pico-satellite[J]. 信息与电子工程前沿(英文), 2012,13(2):83-89.
Yu ZHANG, Yang-ming ZHENG, Mu YANG, et al. Design and implementation of the highly-reliable, low-cost housekeeping system in the ZDPS-1A pico-satellite[J]. Frontiers of Information Technology & Electronic Engineering, 2012, 13(2): 83-89.
Design and implementation of the highly-reliable, low-cost housekeeping system in the ZDPS-1A pico-satellite[J]. 信息与电子工程前沿(英文), 2012,13(2):83-89. DOI: 10.1631/jzus.C1100079.
Yu ZHANG, Yang-ming ZHENG, Mu YANG, et al. Design and implementation of the highly-reliable, low-cost housekeeping system in the ZDPS-1A pico-satellite[J]. Frontiers of Information Technology & Electronic Engineering, 2012, 13(2): 83-89. DOI: 10.1631/jzus.C1100079.
Design and implementation of the highly-reliable, low-cost housekeeping system in the ZDPS-1A pico-satellite
The ZDPS-1A pico-satellite designed in Zhejiang University with a mass of 3.5 kg and a power consumption of less than 3.5 W is the smallest satellite in China up to now. The housekeeping system (HKS) is the core part of ZDPS-1A. The reliability of HKS has an important influence on the safety of the satellite. Traditional fault-tolerant methods do not apply to ZDPS-1A due to such pico-satellite characteristics as light weight
compactness in size
energy saving
and high integration. This paper deals with a highly-reliable
low-cost design for HKS using industrial devices. The reliable strategies of HKS include a dual modular redundancy scheme
CPU warm backup
a static triple modular redundancy scheme
and two-level watchdogs. Recursive experiments
special tests
and environmental tests show that this system meets the design target. This design has already been applied to ZDPS-1A
which was launched to execute in-orbit tasks on Sept. 22
2010. To date
the satellite has been in a proper state for more than 15 months.
关键词
Keywords
references
J.D. Eric , , , K.S. Morgan , , , M.J. Wirthlin , , , M.P. Caffrey , , , P.S. Graham . . Detection of Configuration Memory Upsets Causing Persistent Errors in SRAM-Based FPGAs. LA-UR-04-7085 . . Los Alamos National Laboratory, Los Alamos , , 2004 . . .
R. Funase , , , E. Takei , , , Y. Nakamura , , , M. Nagai , , , A. Enokuchi , , , Y. Cheng , , , K. Nakada , , , Y. Nojiri , , , F. Sasaki , , , T. Funane , , , T. Eishima , , , S. Nakasuka . . Technology Demonstration on University of Tokyo's Pico-satellite "Ⅺ-Ⅴ" and Its Effective Operation Result Using Ground Station Network . . Department of Aeronautics and Astronautics, University of Tokyo, Japan , , 2007 . . .
R.J. Hamann , , , C.J.M. Verhoeven , , , A.R. Bonnema . . Nano-satellites, a Fast Way to Pre-qualify New Micro- technology . . Int. Conf. on MEMS, NANO and Smart Systems , , 2005 . . p.263 - - 264 . . DOI: 10.1109/ICMENS.2005.80 http://doi.org/10.1109/ICMENS.2005.80 . .
P.A. Lashomb . . Triple Modular Redundant (TMR) Microprocessor System for Field Programmable Gate Array (FPGA) Implementation . . MS Thesis, Naval Postgraduate School, Monterey, California , , 2002 . . .
X. Ma . . Design of Housekeeping System with Fault Tolerance Techniques and Studies up the Reliability of Small Satellite . . PhD Thesis, Institute of Technology, Harbin, China (in Chinese) , , 2002 . . .
P. Majewicz . . Implementation of a Configurable Fault Tolerant Processor (CFTP) Using Internal Triple Modular Redundancy (TMR) . . MS Thesis, Naval Postgraduate School, Monterey, California, USA , , 2005 . . .
T. Meng , , , H. Wang , , , Z. Jin , , , K. Han . . Attitude stabilization of a pico-satellite by momentum wheel and magnetic coils . . J. Zhejiang Univ.-Sci. A , , 2009 . . 10 ( ( 11 ): ): 1617 - - 1623 . . DOI: 10.1631/jzus.A0820425 http://doi.org/10.1631/jzus.A0820425 . .
C.S. Mills , , , G. Hines , , , K.R. Fowler , , , M.A. Garrison-Darrin , , , R.F. Conde , , , H.A.C. Eaton . . Adaptive Data Analysis and Processing Technology (ADAPT) for Spacecraft . . NASA Langley Research Center, Electronic Systems Brand, System Engineering Competency, Hampton , , 2003 . . .
F. Qu , , , G. Cui , , , X. Yang , , , X. Tang . . The design and implementation of EDAC module in the house-keeping computer system of TS-1.1 . . Comput. Eng. Sci. , , 2002 . . 24 ( ( 2 ): ): 70 - - 76 . . . .
K. Schilling . . Design of pico-satellites for education in systems engineering . . IEEE Aerosp. Electron. Syst. Mag. , , 2006 . . 21 ( ( 7 ): ): S9 - - S14 . . DOI: 10.1109/MAES.2006.1684269 http://doi.org/10.1109/MAES.2006.1684269 . .
M. Schmidt , , , K. Schilling . . An extensible on-board data handling software platform for pico satellites . . Acta Astronaut. , , 2008 . . 63 ( ( 11-12 ): ): 1299 - - 1304 . . DOI: 10.1016/j.actaastro.2008.05.017 http://doi.org/10.1016/j.actaastro.2008.05.017 . .
D. Schor , , , J. Scowcroft , , , C. Nichols , , , W. Kinsner . . A Command and Data Handling Unit for Pico-satellite Missions . . Canadian Conf. on Electrical and Computer Engineering , , 2009 . . p.874 - - 879 . . DOI: 10.1109/CCECE.2009.5090254 http://doi.org/10.1109/CCECE.2009.5090254 . .
M.N. Sweeting . . Space at Surry: micro-mini-satellites for affordable access to space . . Air Space Eur. , , 2000 . . 2 ( ( 1 ): ): 38 - - 52 . . DOI: 10.1016/S1290-0958(00)80009-X http://doi.org/10.1016/S1290-0958(00)80009-X . .
T. Vladimirova , , , M.N. Sweeting . . System-on-a-chip development for small satellite onboard data handling . . System , , 2008 . . 17 ( ( 1 ): ): 30 - - 35 . . . .
L. Xiang , , , A. Wu , , , M. Liao , , , X. Yang . . Fault-tolerant mechanisms of house-keeping computer system for the small satellite . . J. Astronaut. , , 2005 . . 26 ( ( 4 ): ): 400 - - 404 . . . .
Xilinx . . Radiation Effects & Mitigation Overview . . Available from http://www.xilinx.com/esp/mil_aero/collateral/presentations/radiation_effects.pdf http://www.xilinx.com/esp/mil_aero/collateral/presentations/radiation_effects.pdf , , 2004 . . .
The trial reading is over, you can activate your VIP account to continue reading.