首页> 外文会议>AICI 2011;International conference on artificial intelligence and computational intelligence >Multi-satellite Combined Orbit Determination Parameterized Fusion Model and Weighting Iterativ Estimation Algorithm
【24h】

Multi-satellite Combined Orbit Determination Parameterized Fusion Model and Weighting Iterativ Estimation Algorithm

机译:多卫星联合定轨参数化融合模型和权重迭代估计算法

获取原文

摘要

For multi-LEO combined orbit determination (COD) satellite-network based on space-based tracking telemetry and command (STTC) satellites, kinematic orbit information can be obtained only using the method of precise point positioning (PPP) based on observation models, but the orbits results are not very precise because that the precision of observation data and the Geometry Dilution of Precision (GDOP) of STTC constellation cannot meet the demands of high precision application requirements of LEOs. The high precision denotation model of satellite orbit dynamics based on physics parameter model and mathematics model which associates sparse parameter representation with time sequence analysis, nonlinear semi-parametric combined observation model based on system error parameters modeling and non-parametric component denotation of model error, and COD parameterized fusion model are established aiming at multi-satellite high precision COD based on bi-satellite positioning system and low earth orbiters (LEOs). Then parameters estimation algorithms of the former two kinds of models and the combined estimation algorithm of parameterized fusion model are designed. Theoretic analysis and simulated computation results show that the high precision denotation method of sparse parameters model and the optimized modeling method of observation model considering model error can improve modeling precision, and combined estimation algorithm of parameterized fusion model can synchronously ameliorate orbit determination precision ulteriorly.
机译:对于基于空基跟踪遥测和指挥(STTC)卫星的多LEO组合轨道确定(COD)卫星网络,只能使用基于观测模型的精确点定位(PPP)方法获得运动轨道信息,但是轨道结果不是很精确,因为STTC星座的观测数据的精度和几何精度的几何稀释度(GDOP)不能满足LEO的高精度应用要求。基于物理参数模型和数学模型的卫星轨道动力学高精度表示模型,该模型将稀疏参数表示与时序分析相关联,基于系统误差参数建模的非线性半参数组合观测模型以及模型误差的非参数成分表示,针对基于双卫星定位系统和低地球轨道器(LEOs)的多卫星高精度COD,建立了COD参数化融合模型。然后设计了前两种模型的参数估计算法和参数化融合模型的组合估计算法。理论分析和仿真计算结果表明,稀疏参数模型的高精度表示方法和考虑模型误差的观测模型的优化建模方法可以提高建模精度,参数化融合模型的组合估计算法可以同时改善轨道确定精度。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号