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基于地籍测量的惯性系统初始对准方法研究

Study on Initial Alignment of Inertial System Based on Cadastral Surveying
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摘要 地籍测量过程中具有静态、可调平和转位的特点,在静基座条件下,捷联惯性测量系统(SIMS)粗对准的失准角与卡尔曼滤波精对准的失准角相当,但是解析粗对准的方位角误差较大。本文在建立SIMS静基座粗对准误差方程的基础上,对影响解析粗对准精度的误差因素进行分析,提出利用光纤陀螺寻北仪进行四位置转位寻北的方法来估算方位角的精度,以提高方位角的估计精度。仿真结果表明,该方法可以有效地提高对准精度,适合于静基座外界干扰小的捷联式惯性测量系统上,在一定程度上可以直接作为对准的结果用于地籍测量定位解算。 Cadastral surveying process has features of static, adjustable and translocation. In the stationary base conditions, the misalignment angles of coarse alignment of Inertial Measurement System (SIMS) parallel fairly with the misalignment angles of fine alignment of Kalman Filter, but the azimuth error of coarse alignment is larger. On the basis of establishing the error equations of analytic coarse alignment for SIMS on stationary base, this paper analyzes the factors that affect the precision of coarse alignment error, puts forward to using the method of four position found north to estimate the accuracy of the azimuth, to improve the estimation accuracy of azimuth. The simulation results show that compared with the coarse alignment result, this method can effectively improve the alignment accuracy, suitable for the stationary base and small interference of SIMS, which, to a certain degree, can be directly used as a result of the alignment of cadastral surveying positioning algorithm.
出处 《测绘与空间地理信息》 2014年第9期46-49,共4页 Geomatics & Spatial Information Technology
基金 科技部支撑计划--村镇空间规划地理信息快速测高与精确定位技术研究(2012BAJ22B01)资助
关键词 静基座 地籍测量 捷联惯性测量系统 解析粗对准 四位置 stationary base cadastral survey SIMS analytic coarse alignment four - position
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  • 1高伟,郝燕玲,蔡同英.摇摆状态下捷联惯导系统初始对准技术的研究[J].中国惯性技术学报,2004,12(3):15-19. 被引量:10
  • 2秦永元,严恭敏,顾冬晴,郑吉兵.摇摆基座上基于信息的捷联惯导粗对准研究[J].西北工业大学学报,2005,23(5):681-684. 被引量:132
  • 3高茂林,赵忠,张钧.二位置陀螺寻北仪及转位误差分析[J].计算机测量与控制,2006,14(1):70-71. 被引量:20
  • 4王立冬,王夏霄,张春熹.光纤陀螺寻北仪多位置寻北误差分析[J].压电与声光,2007,29(1):42-44. 被引量:21
  • 5Savage P G. Strapdow n inertial navigation system algorithm design, part Ⅱ : velocity and position algorithms[J]. AIAA Journal of Guidance, Control and Dynamics, 1998, 21(2) : 208 - 221.
  • 6Napo Litano F, Oaiffe T, Cot Treau Y, et al. PH INS2 the first high performances inertial navigation system based on fiber optic gyro scopes [ C ]//9th Saint Petersburg International Conference on Integrated Navigation Systems. Saint Petersburg, 2002:296 - 304.
  • 7Savage P G. Strap-down inertial navigation system algorithm design, part Ⅰ: attitude algorithms[J]. AIAA Journal of Guidance, Control and Dynamics, 1998, 21 (1) : 19 - 28.
  • 8曾宗伟.二频机械抖动激光陀螺寻北仪部分关键技术研究[D].长沙:国防科技大学,2006:8-12.
  • 9贾沛璋.误差分析与数据处理[M].北京:国防工业出版社,1999.
  • 10Jiang Yeonfuh,IEEE Trans Aerospace Electronic Systems,1998年,34卷,1期,334页

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