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舰船捷联惯导传递对准仿真验证系统设计 被引量:2

Realization of transfer alignment simulation and verification system for shipborne strapdown inertial navigation system
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摘要 为解决船用捷联惯导系统传递对准仿真中载体机动方式与实际差别较大的问题,提出了基于舰船空间运动的传递对准精度考核的仿真验证系统,提高载体机动方式仿真逼真度。仿真验证系统通过舰船空间运动建模,提供接近真实运动环境的空间运动参数;通过设计空间变换算法,实现了空间运动参数与主惯导惯性器件模拟输入的转化;通过杆臂及挠曲变形计算,实现了子惯导惯性器件模拟输入的转化;文中给出了各模块的算法及解算流程。"速度+姿态"传递对准算法仿真验证结果为10 s内水平失准角精度优于0.02;方位失准角精度优于0.05。仿真验证试验结果表明了该方案的可行性和实用性,该方案为其他领域的传递对准方案分析及验证提供了有效的参考依据。 A transfer alignment simulation and verification scheme based on the ship motion is proposed to improve the simulation fidelity for shipborne inertial navigation system.Compared with conventional schemes,the new scheme can bring motion parameters that are more close to actual motion environment by using the 6-degree of freedom ship motion.The designed space transform algorithm realizes the transform between space motion parameters and analogy input of main inertial navigation devices.The transform of analogy input for slave SINS devices is realized by the calculation of logical lever arm and carrier flexure.The algorithms and solution procedures of each model are given.The velocity plus attitude matching algorithm can reach 0.02 of horizontal angle and 0.05 of azimuth angle in 10 s.The simulation result shows that the scheme is feasible and practical,and can also provide references for the analysis and verification of transfer alignment schemes in other fields.
出处 《中国惯性技术学报》 EI CSCD 北大核心 2011年第6期642-647,共6页 Journal of Chinese Inertial Technology
基金 国家973重大基础研究项目(61312101)
关键词 舰船空间运动 捷联惯导 传递对准 杆臂 弹性变形 ship space motion SINS transfer alignment level arm carrier flexure
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参考文献9

  • 1Shen Xiaorong, Shi Yongzhu, Angular rate matching method for shipboard transfer alignment based on H filter[C]// 2011 the 6th IEEE Conference on Industrial Electronics and Applications (ICIEA). 21-23 June 2011: 620-625.
  • 2王司,邓正隆.惯导系统动基座传递对准技术综述[J].中国惯性技术学报,2003,11(2):61-67. 被引量:64
  • 3王司,邓正隆.一种新的动基座快速传递对准方案及其仿真研究[J].宇航学报,2005,26(3):321-325. 被引量:7
  • 4Chaudhuri S K, Nandi P K. Transfer alignment for space vehicles launched from a moving base[J]. Defense Science Journal, 2005(3): 245-252.
  • 5Zhao L, Yan L, Cheng J H. The research of inertial navigation system based on submarine space motion[C]//2008 IEEE Pacific-Asia Workshop on Computational Intelligence and Industrial Application (PACIIA 2008). Wuhan, China, 19-20 Dec, 2008: 751-755.
  • 6张秀凤,尹勇,金一丞.规则波中船舶运动六自由度数学模型[J].交通运输工程学报,2007,7(3):40-43. 被引量:60
  • 7Cheng Jian-hua, Shi Jun-yu. The research of INS's error analysis for underwater vehicle in complex sea conditions[C]// The 8th World Congress on Intelligent Control and Automation(WCICA). Jinan, Shandong, China, July 6 - 9, 2010: 3445-3449.
  • 8李璞,王丹丹,王丽华.速度加姿态匹配的传递对准算法研究[J].导弹与航天运载技术,2009(5):9-12. 被引量:4
  • 9Xu Qingjiu, Dai Hongde. Design of simulation system about transfer alignment of SINS for shipbome equipment[C]// 2010 2^nd International Conference on Information Science and Engineering(ICISE). 4-6 Dec. 2010: 4506-4510.

二级参考文献51

  • 1黄国,刘天威,严乃长,楼连根.船舶在规则波中回转运动的研究[J].上海交通大学学报,1996,30(10):152-158. 被引量:6
  • 2Shortelle K J, Graham W R, Rabourn C. F-16 flight tests of a rapid transfer alignment procedure[C]. IEEE Position Location and Navigation Symposium. 1998:379-386.
  • 3Kain J E, Cloutier J R. Rapid transfer alignment for tactical weapon applications[R]. AIAA-89-3581, 1989.
  • 4Alan M. Schneider. Kalman filter formulation for transfer alignment of strap-down inertial units[J]. Navigation: Journal of the Institute of Navigation, 1983,30(1 ).
  • 5Tarrant D, Roberts C, Jones D,et al. Rapid and robust transfer alignment[A]. IEEE Proceedings of Aerospace Control Systems[C], 1993: 758-762.
  • 6Klotz H A Jr, Derbak C B. GPS-aided navigation and unaided navigation on the joint direct attack munition[A]. IEEE Position Location and Navigation Symposium[C], 1998: 412-419.
  • 7Kain J E, Cloutier J R. Rapid transfer alignment for tactical weapon applications[R]. AIAA-89-3581.
  • 8Shortelle K J, Graham W R, Rabourn C. F-16 flight tests of a rapid transfer alignment procedure[A]. IEEE Position Location and Navigation Symposium[C], 1998:379-386.
  • 9Graham W R, Shortelle K J. Rapid alignment prototype (RAP) flight test demonstration[A]. System Dynamics International[R]. 1997, No. ISG-97-01: 30.
  • 10Graham W R. Rapid alignment prototype (RAP) flight test demonstration[A]. Proceedings of the Institute of Navigation (ION) National Technical Meeting[C], 1998.

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