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Airborne SAR system for determining the topography of a terrain

  • US 5,489,907 A
  • Filed: 09/23/1994
  • Issued: 02/06/1996
  • Est. Priority Date: 09/24/1993
  • Status: Expired due to Fees
First Claim
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1. A terrain-mapping airborne synthetic aperture radar system for an aircraft travelling in an x-axis direction of flight at a z-axis elevation over a target, the target being a point of terrain, the x-axis direction being transverse to a y-axis direction;

  • the system comprising;

    a monopulse radar antenna including a set of radiating elements, the x-axis direction lying within the antenna plane, the antenna plane being inclined to the z-axis direction at an angle α

    ;

    means for distributing radar pulses to the radiating elements in a way that radiating elements are separated into two antenna halves in the antenna plane above and below a symmetry line parallel to the x-axis direction;

    on a transmitting side, means for distributing radar pulses to the antenna halves such that the antenna halves transmit the pulses in phase;

    means for detecting echo pulses returned from the target to the radiating elements to generate return signals therefrom;

    first processing means for determining a target range by an echo delay of the return signals;

    second processing means for determining an azimuthal target bearing by detecting a doppler shift of the return signals; and

    third processing means for means for determining a elevational target bearing;

    the third processing means further comprising;

    on a receiving side, phase-shifting means for alternately phase-shifting by a phase angle φ

    , and not phase-shifting, received signals from the two antenna halves;

    imaging means for generating two distinct synthetic-aperture radar images, the images includingan out-of-phase image corresponding to a phase-shifted sequence of returned signals phase shifted by the phase angle φ

    of signals from the two antenna halves andan in-phase image corresponding to a non-shifted sequence of returned signals received without phase-shifting of signals from the two antenna halves;

    dividing means for taking a quotient of intensities of corresponding target image pixels of selectively the in-phase image and the out-of-phase image, the quotient being a function of φ and

    a nadir target bearing angle θ

    between the z-axis direction and the target; and

    angle-determining means for determining from the quotient a nadir target bearing angle θ

    between the z-axis direction and the target, θ

    being equal to 90 degrees-α

    ;

    whereby the ground topography may be determined as a map of target image pixels in three dimensions of range, azimuthal angle, and nadir angle.

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