• DocumentCode
    8270
  • Title

    Adaptive pinpoint and fuel efficient mars landing using reinforcement learning

  • Author

    Gaudet, Brian ; Furfaro, Roberto

  • Author_Institution
    Dept. of Syst. & Ind. Eng., Univ. of Arizona, Tucson, AZ, USA
  • Volume
    1
  • Issue
    4
  • fYear
    2014
  • fDate
    Oct. 2014
  • Firstpage
    397
  • Lastpage
    411
  • Abstract
    Future unconstrained and science-driven missions to Mars will require advanced guidance algorithms that are able to adapt to more demanding mission requirements, e.g. landing on selected locales with pinpoint accuracy while autonomously flying fuel-efficient trajectories. In this paper, a novel guidance algorithm designed by applying the principles of reinforcement learning (RL) theory is presented. The goal is to devise an adaptive guidance algorithm that enables robust, fuel efficient, and accurate landing without the need for off line trajectory generation and real-time tracking. Results from a Monte Carlo simulation campaign show that the algorithm is capable of autonomously following trajectories that are close to the optimal minimum-fuel solutions with an accuracy that surpasses that of past and future Mars missions. The proposed RL-based guidance algorithm exhibits a high degree of flexibility and can easily accommodate autonomous retargeting while maintaining accuracy and fuel efficiency. Although reinforcement learning and other similar machine learning techniques have been previously applied to aerospace guidance and control problems (e.g., autonomous helicopter control), this appears, to the best of the authors knowledge, to be the first application of reinforcement learning to the problem of autonomous planetary landing.
  • Keywords
    Monte Carlo methods; adaptive control; aerospace control; learning (artificial intelligence); space vehicles; trajectory control; Mars landing; Monte Carlo simulation; RL theory; RL-based guidance algorithm; adaptive guidance algorithm; aerospace control; aerospace guidance; autonomous planetary landing; machine learning techniques; mission requirements; realtime tracking; reinforcement learning; science-driven mission; trajectory generation; Algorithm design and analysis; Atmospheric modeling; Learning (artificial intelligence); Mars; Mathematical model; Space missions; Space vehicles; Trajectory; Markov decision process; Mars landing guidance; policy iteration; reinforcement learning;
  • fLanguage
    English
  • Journal_Title
    Automatica Sinica, IEEE/CAA Journal of
  • Publisher
    ieee
  • ISSN
    2329-9266
  • Type

    jour

  • DOI
    10.1109/JAS.2014.7004667
  • Filename
    7004667