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Attitude Determination Algorithm Based on Antenna Configuration |
CUI Jianhua①② CHENG Naiping① |
①(Academy of Equipment, Beijing 101416, China)
②(Unit 66407 of PLA, Beijing 100144, China) |
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Abstract In order to solve the problem of high computational complexity of the ambiguity in attitude measurement, a new attitude measurement method based on antenna configuration is proposed. In a certain range of measurement error, the antenna array for attitude determination is properly configured, the integer ambiguity of double difference carrier phase is determined by the constraint information of antenna configuration. Short-baseline and middle-baseline are used for coarse and precise attitude measurement. This method for aerocraft attitude determination does not need to solve the ambiguity. It avoids the use of complex ambiguity search algorithm and improves the speed of attitude determination, it is suitable for fast attitude measurement of aerocraft.
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Received: 11 April 2016
Published: 17 October 2016
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Corresponding Authors:
CUI Jianhua
E-mail: cjh_xilinx@163.com
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[1] |
许江宁, 朱涛, 卞鸿巍. GPS姿态测量技术综述[J]. 海军工程大学学报, 2003, 15(3): 17-22. doi: 10.3969/J.ISSN.1009-3486. 2003.03.005.
|
|
XU Jiangning, ZHU Tao, and BIAN Hongwei. Review on GPS attitude determination[J]. Journal of Naval University of Engineering, 2003, 15(3): 17-22. doi: 10.3969/J.ISSN. 1009-3486.2003.03.005.
|
[2] |
徐定杰, 党超, 沈锋. 一种解算整周模糊度几何算法实现GPS快速测姿[J]. 宇航学报, 2011, 32(12): 2518-2525. doi: 10. 3873/J.ISSN.1000-1328.2011.12.008。
|
|
XU Dingjie, DANG Chao, and SHEN Feng. A geometric method for integer ambiguity solution in GPS attitude determination[J]. Journal of Astronautics, 2011, 32(12): 2518-2525. doi: 10.3873/J.ISSN.1000-1328.2011.12.008.
|
[3] |
CHIANG K, PSIAKI M, and POWELL S. GPS-based attitude determination for a spinning rocket[J]. IEEE Transactions on Aerospace and Electronic Systems, 2014, 50(4): 2654-2663. doi: 10.1109/TAES.2014.120822.
|
[4] |
OLIAZADEH N, LANDRY R, and YESTE-OJEDA O A. GPS-based attitude determination using RLS and LAMBDA methods[C]. IEEE 2015 International Conference on Localization and GNSS (ICL-GNSS). Gothenburg, Sweden, 2015: 1-7. doi: 10.1109/ICL-GNSS.2015.7217146.
|
[5] |
KIS L and LANTOS B. Aided carrier phase differential GPS for attitude determination[C]. 2011 IEEE ASME International Conference on Advanced Intelligent Mechatronics (AIM). Budapest, Hungary, 2011: 778-783. doi: 10.1109/AIM.2011.6027009.
|
[6] |
NADARAJAH N, TEUNISSEN P J G, and RAZIQ N. Instantaneous GPS-Galileo attitude determination: single- frequency performance in satellite-deprived environments[J]. IEEE Transactions on Vehicular Technology, 2013, 62(7): 2963-2976. doi: 10.1109/TVT.2013.2256153.
|
[7] |
田增山, 胡小川, 刘丽川。GPS姿态测量系统基线长度和天线布局设计[J]. 电波科学学报, 2001, 16(3): 379-383. doi: 10. 3969/J.ISSN.1005-0388.2001.03.021。
|
|
TIAN Zengshan, HU Xiaochuan, and LIU Lichuan. The design of baseline length and antenna configuration for GPS attitude determination system[J]. Chinese Journal of Radio Science, 2001, 16(3): 379-383. doi: 10.3969/J.ISSN.1005- 0388.2001.03.021.
|
[8] |
ARDALAN A A and REZVANI M H. An iterative method for attitude determination based on misaligned GNSS baselines[J]. IEEE Transactions on Aerospace and Electronic Systems, 2015, 51(1): 97-107. doi: 10.1109/TAES.2014. 130070.
|
[9] |
TATIYAWORANUN C and PURIVIGRAIPONG S. An operational algorithm for satellite attitude determination from GPS carrier phase[C]. IEEE 2012 9th International Conference on Electrical Engineering/Electronics, Computer, Telecommunications and Information Technology (ECTI-CON), Hua Hin, Thailand, 2012: 1-4. doi: 10.1109/ ECTICon.2012.6254194.
|
[10] |
KOZLOV A, GOLOVAN A, NIKULIN A, et al. GPS attitude determination under antenna array geometry deformation[C]. 7th International Conference on Recent Advances in Space Technologies. Istanbul, Turkey, 2015: 713-717. doi: 10.1109/ RAST.2015.7208434.
|
[11] |
SCATAGLINI T, PAGOLA F, COGO J, et al. Attitude estimation using GPS varrier phase single differences[J]. IEEE Latin America Transactions, 2014, 12(12): 847-852. doi: 10.1109/TLA.2014.6872894.
|
[12] |
COIAS J, SANGUINO J, and OLIVEIRA P. Attitude determination using the ambiguity filter with single-frequency L1 GPS receivers[C]. 2012 International Conference on Localization and GNSS (ICL-GNSS). Starnberg, Germany 2012: 1-6. doi: 10.1109/ICL-GNSS. 2012.6253133.
|
[13] |
刘根友, 欧吉坤. GPS单历元定向和测姿算法及其精度分析[J]. 武汉大学学报:信息科学版, 2003, 28(6): 732-735. doi: 10.3321/J.ISSN:1671-8860.2003.06.024
|
|
LIU Genyou and OU Jikun. Determining attitude with single epoch GPS algorithm and its precision analysis[J]. Editorial Board of Geomatics & Information Science of Wuhan University, 2003, 28(6): 732-735. doi: 10.3321/J.ISSN:1671- 8860.2003.06.024
|
[14] |
杨铁军, 张晓玲, 付毓生, 等. 基于DSP的GPS双天线实时姿态测量系统实现[J]. 电波科学学报, 2002, 17(6): 661-665. doi: 10.3969/J.ISSN.1005-0388.2002.06.024.。
|
|
YANG Tiejun, ZHANG Xiaoling, FU Yusheng, et al. Implementation of GPS twin antennas real-time attitude determination system based on DSP[J]. Chinese Journal of Radio Science, 2002, 17(6): 661-665. doi: 10.3969/J.ISSN. 1005-0388.2002.06.024.
|
[15] |
HENKEL P and IAFRANCESCO M. Tightly coupled position and attitude determination with two low-cost GNSS receivers[C]. 2014 IEEE 11th International Symposium on Wireless Communications Systems (ISWCS), Barcelona, Spain, 2014: 895-900. doi: 10.1109/ISWCS.2014.6933480.
|
[16] |
茅文深, 常传文. 基于导航卫星的载体姿态测量[M]. 北京:国防工业出版社, 2015: 26-35.
|
|
MAO Wenshen and CHANG Chuanwen. Carrier Attitude Measurement Based on Navigation Satellite[M]. Beijing: National Defense Industry Press, 2015: 26-35.
|
|
|
|