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Extended Integrative Combined Orbit Determination Models based on Sparse Parameters Representation and Combined Optimal Weighting Algorithm

机译:基于稀疏参数表示和组合最优加权算法的扩展综合组合轨道确定模型

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For multi-satellite combined orbit determination (COD) network system based on GEO-IGSO-MEO satellite constellation and LEOs, the to-be-estimated satellites trajectory parameters results are not very precise because of satellites orbit perturbation indefinable physical models, observation models without adequately considering model error or measure mixed error, imprecise parameters estimation algorithm or linear least squares (LS) estimation algorithm, which cannot meet high precision application requirements of LEOs. Firstly, the high precision sparse parameters representation model of GEO-IGSO-MEO and LEOs orbit dynamics model is proposed. Above on this, the extended integrative COD models which combine parametric modeling and semi-parametric component representation based on measurement systematic errors and model errors are proposed. Secondly, the paper proposed weighting iterative wavelet estimation method of dynamics sparse parameters representation model, and LS approximation estimation method of non linear semi-parametric model is designed based on above models. Lastly, combined optimal weighting parameters estimation algorithm of extended integrative COD models which combines parametric estimation and non-parametric estimation are designed. Theoretic analysis and simulated computation results show that if only the physical model is used for COD, there is relatively big dynamical modeling error between dynamical model implied and the actual, which LEO precision cannot meet application requirements. When the high precision representation method of sparse parameters model and the optimized modeling method of observation model considering model errors can improve modeling and parameters estimation precision, and parameterized system error, model error and model parameters are estimated by extended integrative COD synchronously, so the orbit determination precision of LEOs can be improved evidently.
机译:对于基于GEO-IGSO-MEO卫星星座和LEO的多卫星联合定轨(COD)网络系统,由于卫星的轨道扰动无法定义物理模型,而没有观测模型,观测卫星的轨道参数结果不是很精确。充分考虑模型误差或度量混合误差,不精确的参数估计算法或线性最小二乘(LS)估计算法,这些算法无法满足LEO的高精度应用要求。首先,提出了GEO-IGSO-MEO的高精度稀疏参数表示模型和LEOs轨道动力学模型。在此之上,提出了基于测量系统误差和模型误差的参数化建模和半参数化组件表示相结合的扩展集成化COD模型。其次,提出了动态稀疏参数表示模型的加权迭代小波估计方法,并在上述模型的基础上设计了非线性半参数模型的LS近似估计方法。最后,设计了结合参数估计和非参数估计的扩展集成COD模型的最优加权参数估计算法。理论分析和仿真计算结果表明,如果仅将物理模型用于COD,则隐含的动力学模型与实际模型之间存在较大的动力学建模误差,LEO精度不能满足应用要求。当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和参数估计精度,并且参数化系统误差,模型误差和模型参数通过扩展集成COD同步估计时,轨道LEO的测定精度可以明显提高。

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