A new type of navigation system that meets the navigation requirements of deep space exploration missions with strong autonomous operation capability has become an urgent need. This paper proposes a new type of navigation constellation which has the characteristics of long-term stability under the full force model. Previously, we have studied that the orbits of the navigation constellation can be determined autonomously using the inter-satellite range data. As a continuation of the previous study, this article mainly studies the autonomous navigation performance of the navigation constellation under the actual force model. Here, the lunar probe’s mission of the Earth-Moon transition section is taken as an example, the observation data is inter-satellite ranging. When the ranging error is 1 m, the navigation constellation realizes autonomous navigation of the earth-moon transition section detector, and the navigation accuracy is within 1 m. The accuracy requirements are met. The current study can be used when deploying the navigation constellation in the Earth-Moon system.


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    Title :

    Autonomous Navigation Based on Dynamical Substitutes in the Earth-Moon System Under the Full Force Model


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Yan, Liang (editor) / Duan, Haibin (editor) / Deng, Yimin (editor) / Liu, Bin (author) / Fang, Yanan (author) / Wang, Chong (author) / Zhang, Zhibin (author) / Wang, Jingyan (author)

    Conference:

    International Conference on Guidance, Navigation and Control ; 2022 ; Harbin, China August 05, 2022 - August 07, 2022



    Publication date :

    2023-01-31


    Size :

    7 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English