• DocumentCode
    622653
  • Title

    Planner test and analyzing system for deep space mission

  • Author

    Fanyu Zhao ; Pingyuan Cui ; Rui Xu ; Ting Peng ; Dexiang Chen

  • Author_Institution
    Beijing Inst. of Technol., Beijing, China
  • fYear
    2013
  • fDate
    12-14 June 2013
  • Firstpage
    1224
  • Lastpage
    1229
  • Abstract
    As deep space exploration develops, onboard autonomy capability of the explorer becomes increasingly important, which requires the onboard planner to be more efficient. To improve the autonomy, a ground-based real-time fidelity simulation environment is needed, which enables rapid integration, testing and analyzing of the explorer planner. This paper describes the development of a Planner Test and Analysis System (PTAS) based on exploration mission. The planner modules under development include flight software, dynamic models, data interfaces, and monitoring module. Unified interface has been designed for application of planners with system level integration. The flight software includes attitude control subsystem, autonomous navigation, trajectory computing subsystem, and execution control subsystem. Planning result is analyzed by the flight software into executable commands on the embedded computer, and then transmitted to dynamic models on the multi-CPU computer, which makes PTAS a hardware-in-loop system. With some interfaces users could configure their own dynamic models. Simulation status about the explorer states and the process of mission simulation could be monitored, while planning and execution results could be analyzed quantitatively through a graphical interface, to show the planning efficiency and help users to improve the planner.
  • Keywords
    aerospace computing; attitude control; control engineering computing; digital simulation; graphical user interfaces; mobile robots; multiprocessing systems; path planning; vehicle dynamics; PTAS; analyzing system; attitude control subsystem; autonomous navigation; data interfaces; deep space exploration; deep space mission; dynamic models; execution control subsystem; explorer planner analysis; explorer planner testing; flight software; graphical interface; ground-based real-time fidelity simulation environment; hardware-in-loop system; monitoring module; multiCPU computer; onboard autonomy capability; planner test-and-analysis system; trajectory computing subsystem; Attitude control; Computational modeling; Payloads; Planning; Software; Trajectory;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control and Automation (ICCA), 2013 10th IEEE International Conference on
  • Conference_Location
    Hangzhou
  • ISSN
    1948-3449
  • Print_ISBN
    978-1-4673-4707-5
  • Type

    conf

  • DOI
    10.1109/ICCA.2013.6565124
  • Filename
    6565124