Abstract The Mars atmospheric entry phase plays a vital role in the whole Mars exploration mission-cycle. It largely determines the success of the entire Mars mission. In order to achieve a pin-point Mars landing, advanced entry guidance and control is essential. This paper systematically summarizes the past development and current state-of-art of Mars entry guidance and control technologies. More specifically, the Mars entry process and main technical challenges are first introduced. Second, the guidance and control technologies adopted in the past successful Mars landing mission are reviewed in detail. Next, current state-of-art and recent developments of guidance and control for Mars atmospheric entry are summarized at length. The advantages and disadvantages of the various existing methods are analyzed. Lastly, supposing future Mars pin-point landing missions as the potential project application goals, a more comprehensive outlook and prospect for the next-generation Mars entry guidance and control technologies are described.


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    Titel :

    Review and prospect of guidance and control for Mars atmospheric entry


    Beteiligte:
    Li, Shuang (Autor:in) / Jiang, Xiuqiang (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2014-04-21


    Format / Umfang :

    18 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Schlagwörter :

    AFL , astrobiology field laboratory , MER-B , Opportunity , CG , center of gravity , MSL , Mars science laboratory , CGT , command generator tracker , MSMSG , multiple sliding mode surface guidance , DEKF , desensitized extended kalman filter , MSR , Mars sample return , DOF , degree-of-freedom , MOLA , Mars orbiter laser altimeter , DSN , deep space network , MOPSO , multi-objective particle swarm optimization , EAGLE , evolved acceleration guidance logic for entry , MPF , Mars Pathfinder , EDL , entry, descent and landing , NASA , National Aeronautics and Space Administration , ESA , European Space Agency , NLP , non-linear programming , ETPC , entry terminal point controller , NNSMVSC , neural network-based sliding mode variable structure control , GNC , guidance, navigation and control , NPC , nonlinear predictive controller , HERRO , human exploration using real-time robotic operations , PC , polynomial chaos , IMU , inertial measurement unit , PD , proportional-differential , KKT , Karush–Kuhn–Tucker , PEDALS , parametric entry, descent, and landing synthesis , L/D , lift-to-drag ratio , PWM , pulse-width-modulation , LQR , linear quadratic regulator , RCS , reaction control system , Mars-GRAM , Mars global reference atmospheric model , SAMIC , structured adaptive model inversion control , MCD , Mars climate database , SMVSC , sliding mode variable structure control , MEDLI , MSL entry, descent, and landing instrument , SOPSO , single objective particle swarm optimization , MER , Mars Exploration Rovers , UHF , ultra-high frequency , MER-A , Spirit , Mars atmospheric entry , Guidance and control , Review and prospect





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