• DocumentCode
    2789355
  • Title

    Next generation millimeter-wave radar for safe planetary landing

  • Author

    Pollard, Brian D. ; Sadowy, Gregory

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA
  • fYear
    2005
  • fDate
    5-12 March 2005
  • Firstpage
    1213
  • Lastpage
    1219
  • Abstract
    Safe, precise landing on planetary bodies requires knowledge of altitude and velocity, and may require active detection and avoidance of hazardous terrain. Radar offers a superior solution to both problems due to its ability to operate at any time of day, through dust and engine plumes, and ability to detect velocity coherently. While previous efforts have focused on providing near term solutions to the safe landing problem, we are designing radar velocimeters and radar imagers for missions beyond the next decade. In this paper we identify the fundamental issues within each approach, at arrive at strawman sensor designs at a center frequency at or around 160 GHz (G-band). We find that a G-band radar velocimeter design is capable of sub-10 cm/s accuracy, and a G-band imager is capable of sub-0.5 degree resolution over a 28 degree field of view. From those designs, we arrive at the key technology requirements for the development of power and low noise amplifiers, signal distribution methods, and antenna arrays that enable the construction of these next generation sensors
  • Keywords
    radar imaging; sensors; velocimeters; 160 GHz; G-band radar imager; G-band radar velocimeter; antenna arrays; low noise amplifier; millimeter wave radar; power amplifier; safe planetary landing; signal distribution methods; strawman sensor; Engines; Frequency; Image resolution; Millimeter wave radar; Noise generators; Radar detection; Radar imaging; Sensor arrays; Signal design; Signal resolution;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2005 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    0-7803-8870-4
  • Type

    conf

  • DOI
    10.1109/AERO.2005.1559412
  • Filename
    1559412