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    • 1. 发明专利
    • Synthetic aperture radar device and numerical altitude model creation method
    • JP2004191053A
    • 2004-07-08
    • JP2002355409
    • 2002-12-06
    • Mitsubishi Electric Corp三菱電機株式会社
    • ONO CHIKAKOHORIUCHI KENJI
    • G06T1/00G01S13/90G06T5/00
    • PROBLEM TO BE SOLVED: To provide a synthetic aperture radar device and a numerical altitude model creation method capable of calculating efficient and highly accurate numerical altitude model by detecting a phase noise to an interferogram and by reducing the phase noise by using wavelet transformation when the phase noise is larger than a threshold. SOLUTION: This device is equipped with a means for performing pulse transmission to an observation object, allowing acquired two SAR image data to interfere each other, and generating re-sample data wherein the interference becomes maximum, a means for calculating also the phase difference between either of the two SAR image data and the re-sample data and removing a plane phase to thereby create the interferogram, a means for detecting the phase noise of the interferogram and performing the wavelet transformation to thereby remove the phase noise, a means for developing a phase convoluted in 0-2π by the interferogram into an absolute phase, a means for converting to a high degree the absolute phase as an output from a phase unwrap means, and a means for correcting fore-shortening wherein a projection on the ground seems to fall down into a near range and calculating the numerical altitude model. COPYRIGHT: (C)2004,JPO&NCIPI
    • 2. 发明专利
    • RADAR APPARATUS
    • JPH11248828A
    • 1999-09-17
    • JP4676698
    • 1998-02-27
    • MITSUBISHI ELECTRIC CORP
    • ONO CHIKAKO
    • G01S13/34G01S13/89
    • PROBLEM TO BE SOLVED: To enable practical recognition of a runway by sharpening and finely resolving beams with the use of millimeter waves so as to form an image of the runway and storing data obtained by scanning the beams into a signal- processing part. SOLUTION: A signal transmitted from a transmission part 4 is switched by a circulator 3 to be sent out from an aerial 1 scanned by an aerial-rotating mechanism 2. A reflecting signal from a runway is received by the aerial 1 and switched by the circulator 3 to be received and input to a reception part 5. A distance to the runway is detected by a distance calculation circuit 6 in a signal-processing part 8. The distance data obtained by scanning the aerial is stored in a memory 7, thereby enabling mapping in a range direction. Since the beams are scanned and data are stored in the memory in the signal- processing part thereby forming a high-resolution image of the runway, the runway can be recognized practically.
    • 3. 发明专利
    • SYNTHETIC APERTURE RADAR EQUIPMENT
    • JPH10246779A
    • 1998-09-14
    • JP5027097
    • 1997-03-05
    • MITSUBISHI ELECTRIC CORP
    • ONO CHIKAKOEMA KOUICHIHARA YOSHIHISA
    • G01S7/28G01S7/40G01S13/90
    • PROBLEM TO BE SOLVED: To form a most suitable antenna pattern by providing the specific number of monitor antennas on a satellite because of calculating a deformation amount between the even number of antenna panels. SOLUTION: A signal generated by a signal generator 4 is transmitted and received to a transmitting and receiving module 2 via a transmitter 3 as a transmitting signal 10. For instance, a radio wave transmitted from an antenna 1 composed of four panels is received by five monitor antennas 7 mounted on a satellite. A receiving signal 11 from the antenna 7 is input to a receiver 5, and A/D converted by a data processing part 6 to be transmitted to a control part 8. The part 8 determines five independent parameters of amplitude, a phase, deformation on an X-axis, deformation on a Y-axis and deformation on a Z-axis of each transmitting and receiving module by using the five antennas 7 and performing measurement five times. A setting phase is calculated in consideration to the calculated amplitude, phase, deformation on the X-axis, deformation on the Y-axis and deformation on the Z-axis of each transmitting and receiving module, transmitted to the transmitting and receiving module 2 via an interface 9, and a proper antenna pattern is formed.