Vessel Surface Equipment Attitude Measurement Based on Conventional Inertial Reference System

Abstract:

Vessel weapon firing precision is deeply influenced by the attitude, which also affects vessel combat efficiency. In order to realize the high precision determination of vessel weapon attitude, this paper presented the weapon attitude measuring theory based on CIRS(Conventional Inertial Reference System). The theory contained star apparent place synchronous calculation, star image coordinates calculation and three-axis attitude solution. It was realized that weapon attitude measurement could be carried out in the sailing, which error was not accumulated. The advantage of this theory is high precision, high reliability and low cost.

• Periodical: Advanced Materials Research (Volume 629)
• Pages: 878-883
• DOI: https://doi.org/10.4028/www.scientific.net/AMR.629.878
• Online since: December 2012
• Authors: Lei Zhang, An Guo Wang
• Keywords: Astronomy, Attitude Measurement, CIRS, Reference, Traffic Engineering

References

[1] Lili Ai, Feng Yuan, Zhenliang Ding, Study of the spatial object's exterior attitude measurement based on multi-linear CCD, Industrial Electronics and Applications, ICIEA 3rd IEEE Conference on Digital Object Identifier, 2008 , Page(s): 1945 - (1948).

DOI: 10.1109/iciea.2008.4582859

[2] Yu Chen, Bo Cai, Dengyi Zhang, Xuhui Chen, Peisheng Wu, A novel attitude measurement system base on mems-sensors, Informatics in Control, Automation and Robotics (CAR), 2010 2nd International Asia Conference on Volume: 3, Digital Object Identifier: 10. 1109/CAR. 2010. 5456699, Publication Year: 2010 , Page(s): 327 - 330.

DOI: 10.1109/car.2010.5456699

[3] Pohner F., Steensen I., Precision attitude measurements for survey vessels", OCEANS '94. 'Oceans Engineering for Today's Technology and Tomorrow's Preservation., Proceedings, Volume: 3, Publication Year: 1994 , Page(s): III/545 - III/550 vol. 3.

DOI: 10.1109/oceans.1994.364258

[4] Xu Hui-Gang , Bo Yu-Ming , Analytic solution for the attitude measurement of aerostat via a single camera, Binggong Xuebao/Acta Armamentarii, v 29, n 1, pp.116-120, January (2008).

[5] Balasubramaniam, Senthil, Static attitude measurement system for head suspension assemblies, Hutchinson Technology Incorporated Publication Number: US6747267 Publication date: 06/08/2004 Kind: Utility Patent Grant.

[6] Gedde, Lance D., Quinn, James P., Platform attitude measurement system, Recon/Optical, Inc, 05/12/(1998).

[7] Qin Li, Zhang Wendong, Zhang Huixin Attitude measurement system based on micro-silicon accelerometer array, Chaos, Solitons and Fractals, v 29, n 1, pp.141-147, July (2006).

DOI: 10.1016/j.chaos.2005.08.014

[8] Gilkey James, Richardson David, Terndrup Christopher, Single-baseline attitude measurement system using low-cost C/A-code receivers, Proceedings of ION GPS, v2, pp.1723-1731, (1995).

[9] Xu Hui-Gang, Bo Yu-Ming, Guo Zhi, Analytic solution for the attitude measurement of aerostat via a single camera, Binggong Xuebao/Acta Armamentarii, v29, n1, pp.116-120, January (2008).

[10] Balasubramaniam, Senthil, Static attitude measurement system for head suspension assemblies, Hutchinson Technology Incorporated , 06/08/(2004).

[11] Michael A., Rios Jose, Dynamic attitude measurement method and apparatusHorton, Crossbow Technology Inc, 08/26/(2008).

[12] Song Jin, Rios Jose A., Horton Michael A. Dynamic attitude measurement sensor and method, Crossbow Technology Inc., 07/16/(2002).

[13] Kamimura, Heihachiro, Nishida, Evaluation of attitude measurement using a color marker, Proceedings of SPIE - The International Society for Optical Engineering, v6174II, 2006, Smart Structures and Materials 2006 - Sensors and Smart Structures Technologies for Civil, Mechanical, and Aerospace Systems.

DOI: 10.1117/12.657373

[14] Sun Yong-Rong, Liu Jian-Ye, Chen Wu, vessel attitude system for multibeam echosounding, Journal of Nanjing University of Aeronautics and Astronautics, v35, n4, pp.356-360, August (2003).

[15] Bian Hongwei, Jin Zhihua, Tian Weifeng, Study on GPS attitude determination system aided INS using adaptive Kalman filter, Measurement Science and Technology, v16, n10, pp.2072-2079, October 1, (2005).

DOI: 10.1088/0957-0233/16/10/024