期刊文献+

捷联惯导系统内水平阻尼网络设计 被引量:12

Damp Network Design of Horizontal Loop in Strapdown Inertial Navigation System
下载PDF
导出
摘要 针对捷联惯导系统水平回路的控制系统模型和误差特性,研究系统内水平阻尼网络的设计方法。通过建立单通道水平回路的控制系统模型,分析了系统的稳定性和频率特性。针对幅频特性曲线不同频段表征系统的不同性能,研究了一种基于对数幅频特性曲线的阻尼网络设计方法。通过将系统期望的调节时间、超调量等时域指标转化为频域参数,设计系统期望的开环幅频特性,从而确定捷联惯导系统水平阻尼网络参数。利用本文阻尼网络进行了捷联惯导系统数字仿真和海上试验。仿真条件下系统姿态误差的舒拉周期振荡成分经1~2个舒拉周期后衰减至零,系统位置误差由4 nmile/24 h提高至1.5 nmile/24 h.系统海上阻尼试验结果表明系统姿态精度提高1个数量级,位置精度提高1倍。与试探法设计的网络相比,本文网络具有一致的稳态性和更小的超调量和调节时间。 The damp network design for strapdown inertial navigation system(SINS) was studied according to the control model and error characteristic of SINS horizontal loop.The stability and frequency characteristic of the system was analyzed on the basis of the control model.As the logarithmic magnitude curve of the horizontal loop model on different frequency bands reflected different performance of the system,a design method based on the expected curve was proposed.In the method,the time-domain performance indexes were transformed to frequency parameters,by which the expected logarithmic magnitude curve was plotted.Finally the damp network parameters were obtained.Digital simulation and test on sea for SINS were completed.In the simulation the Schuler oscillation in attitude error was damped to zero and the position error was increased to 1.5 nmile/24 h from 4 nmile/24 h,and in the test on sea the attitude accuracy improved by 1 order and the position accuracy improved by 1 time when the damp network was cascaded into the SINS.Compared with the network designed by the tentative method,this damp network has the same steady-state performances and less overshoot and settling time.
出处 《兵工学报》 EI CAS CSCD 北大核心 2011年第8期996-1001,共6页 Acta Armamentarii
基金 国家自然科学基金(40904018) 中国人民解放军总装备部"探索一代"重大项目(7130529) 教育部重点实验室开放基金资助(201001)
关键词 船舶、舰船工程 捷联惯导 阻尼网络 频率特性 ship engineering strapdown inertial navigation system damp network frequency characteristic
  • 相关文献

参考文献4

二级参考文献21

  • 1杜亚玲,刘建业,刘瑞华,孙永荣.捷联惯性航姿系统中的模糊内阻尼算法研究[J].南京航空航天大学学报,2005,37(3):274-278. 被引量:18
  • 2徐田来,游文虎,崔平远.基于模糊自适应卡尔曼滤波的INS/GPS组合导航系统算法研究[J].宇航学报,2005,26(5):571-575. 被引量:59
  • 3Curey R K, Ash M E, Thielman L O, et al. Proposed IEEE inertial systems terminology standard and other inertial sensor standards[A]. IEEE Position Location Navigation Symposium 2004[C]. Montery,CA, 2004.
  • 4Vanderwerf K. Schuler pumping of inertial velocity errors due to gravity anomalies along a popular North Pacific airway[A]. Position Location and Na-vigation Symposium, IEEE[C]. 1996.642~648.
  • 5Chernodarov A V. Adaptive robust damping of divergent oscillations in updatable inertial systems, control of oscillations and chaos[A]. Proceedings of the 2nd International Conference[C]. 2000,1:133~134.
  • 6Dunyak J, Ihab W, Wunsch D, et al. A theory independent fuzzy probability for system reliability[J]. IEEE Trans on Fuzzy System,1999,7(2):286~294.
  • 7Karyuan C. System failure engineering and fuzzy methodolody: an introductory overview[J]. Fuzzy Sets and System, 1996,83(2):113~133.
  • 8Foulloy L, Galichet S. Fuzzy control with fuzzy inputs, fuzzy systems[J]. IEEE Transactions on Fuzzy System, 2003.437~449.
  • 9Ying H. Practical design of nonlinear fuzzy con-trollers with stability analysis for regulating peocesses with unknown mathematical models[J]. Automatica, 1994,30(7):1185~1195.
  • 10张宗麟.惯性导航与组合导航[M].北京:航空工业出版社,2001.

共引文献36

同被引文献65

引证文献12

二级引证文献19

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部