This article investigates an operational orbit's design and sensitivity analysis for Earth observation (EO) missions in non-sun-synchronous orbits. Sun-synchronous orbits are the primary choice for deploying EO satellites, but in the absence of access to such orbits, alternative options can be considered, including multi-sun-synchronous orbits (MSSO) capable of repeating ground track (RGT).In this research, sets of such orbits are designed, taking into account the defined mission and considering the available altitude and inclination of the orbit. To achieve this, a constrained search problem is formulated, considering the constraints related to the characteristics of multi-sun-synchronicity and repeating ground tracks to search for orbit characteristics.Furthermore, to identify the allowable range of injection errors, a sensitivity analysis of the designed orbit's characteristics has been conducted to assess their sensitivity to uncertainties in injection accuracy during a case study investigation.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Design and sensitivity analysis of an Earth observation mission's operating orbit in the absence of injection into the Sun-synchronous orbit


    Beteiligte:
    Amirreza Kosari (Autor:in) / Asad Saghari (Autor:in) / Masoud Khoshsima (Autor:in)


    Erscheinungsdatum :

    2021




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt




    Magnetospheric Multi-Scale Mission's Orbit Propagation Sensitivity to Navigation Errors (AAS 09-323)

    Carpenter, J.R. / American Astronautical Society / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010


    ORBIT DESIGN FOR EARTH OBSERVATION SPACE MISSIONS

    DI GIORGIO FABIO / FRANCIONI ANDREA / CRICENTI ALESSANDRO | Europäisches Patentamt | 2019

    Freier Zugriff

    Innovative Orbit Design For Earth Observation Space Missions

    DI GIORGIO FABIO / FRANCIONI ANDREA / CRICENTI ALESSANDRO | Europäisches Patentamt | 2015

    Freier Zugriff

    Innovative orbit design for earth observation space missions

    DI GIORGIO FABIO / FRANCIONI ANDREA / CRICENTI ALESSANDRO | Europäisches Patentamt | 2018

    Freier Zugriff

    Innovative orbit design for earth observation space missions

    DI GIORGIO FABIO / FRANCIONI ANDREA / CRICENTI ALESSANDRO | Europäisches Patentamt | 2015

    Freier Zugriff