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  • TALARIS Project Update: Overview of Flight Testing and Development of a Prototype Planetary Surface Exploration Hopper

    Paper number

    IAC-11,A3,2A,7,x9362

    Author

    Mr. Christopher Rossi, Massachusetts Institute of Technology (MIT), United States

    Coauthor

    Ms. Farah Alibay, Massachusetts Institute of Technology (MIT), United States

    Coauthor

    Mr. Phillip Cunio, Massachusetts Institute of Technology (MIT), United States

    Coauthor

    Mr. Joe Morrow, MIT, United States

    Coauthor

    Ms. Sarah Nothnagel, MIT, United States

    Coauthor

    Mr. Ted Steiner, Massachusetts Institute of Technology (MIT), United States

    Coauthor

    Mr. Christopher Han, MIT, United States

    Coauthor

    Mr. Ephraim Lanford, Massachusetts Institute of Technology (MIT), United States

    Coauthor

    Prof. Jeffrey Hoffman, Massachusetts Institute of Technology (MIT), United States

    Year

    2011

    Abstract
    The TALARIS (Terrestrial Artificial Lunar And Reduced GravIty Simulator) project is intended to test GNC (Guidance, Navigation, and Control) algorithms on a prototype planetary surface exploration hopper in a simulated reduced gravity environment.  The vehicle is under development by the Draper Laboratory and MIT in support of developments for the Google Lunar X-Prize.  This paper presents progress achieved since September 2010 in flight testing and vehicle development.
    
    Results are reported for restricted degree of freedom (DOF) tests used to tune GNC algorithms on the path to a full 6-DOF hover-hop flight profile.  These tests include 3-DOF tests on flat surfaces restricted to horizontal motion, and 2-DOF vertical tests restricted to vertical motion and 1-DOF attitude control.  The results of tests leading up to full flight operations are described, as are lessons learned.
    
    Upgrades to the vehicle are described, including a redesign of the power train for the gravity-offset propulsion system and a redesign of key elements of the spacecraft emulator propulsion system.  The integration of flight algorithms into modular flight software is also discussed.  Future test and development plans are outlined, including the planned addition of navigation sensors to improve performance.
    Abstract document

    IAC-11,A3,2A,7,x9362.brief.pdf

    Manuscript document

    IAC-11,A3,2A,7,x9362.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.