The soft-touchdown, “sky-crane” concept employed by the 2009 NASA Mars Science Laboratory mission requires an order-of-magnitude improvement from previous missions in the sensing of vehicle velocity and altitude. This paper describes the development of a new radar “Terminal Descent Sensor” that provides decimeterper-second velocity accuracy while also providing better than 2% range accuracy on six unique beams. This sensor design uses a millimeter-wave center frequency (Ka-band) and pencil beam antennas to achieve the required velocity precision and to overcome the problems that angle-of-arrival errors can cause in velocity reconstruction. Included are discussions of the design concept, driving requirements, hardware architecture, and results from a high fidelity performance simulation.


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    Title :

    A Radar Terminal Descent Sensor for the Mars Science Laboratory mission


    Contributors:


    Publication date :

    2009-03-01


    Size :

    1490158 byte





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English





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