Spacing synchronization process for satellite-machine double-base SAR system

A bistatic, space-based technology that is applied in radio wave measurement systems, radio wave reflection/re-radiation, and re-radiation utilization. It can solve the problem of limited increase in receiving beam speed, difficulty in designing imaging algorithms, and aggravated system space variation characteristics. And other issues

Active Publication Date: 2009-06-24
四川电子科技大学教育发展基金会
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Problems solved by technology

[0006] However, the above scheme has some disadvantages, mainly including: (1) In order to keep the azimuth resolution from being too low, the multiplier of receiving beam velocity is limited, resulting in a short scene length
(2) During the ec

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  • Spacing synchronization process for satellite-machine double-base SAR system
  • Spacing synchronization process for satellite-machine double-base SAR system
  • Spacing synchronization process for satellite-machine double-base SAR system

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Embodiment Construction

[0064] The parameters of the X-band radar satellite TerraSAR-X and the airborne radar PAMIR are used for calculation.

[0065] The flying altitude of the satellite is 515km, the flying speed is 7.6km / s, the antenna gain is 45dB, the antenna viewing angle range is 20°~55°, the transmitting power is 2.26KW, the wavelength is 3.1cm, the duty cycle is 0.18, and the signal bandwidth is 150MHz; the flight altitude of the aircraft is 3km, the antenna gain is 30dB, the antenna angle of view ranges from 40° to 70°, the flight speed is 100m / s, T=260K, F=5dB, L=5dB; σ b 0 = - 20 dB , SNR min = 10dB.

[0066] Firstly, substitute relevant parameters into formula (4) and formula (5), and calculate the allowable reduction multiple of signal-to-noise ratio. Figure 4 Calculation results are given. It can be seen from the figure that at high incident angles, due to the long distance b...

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Abstract

A space synchronous method of a space-borne bi-static SAR system belongs to the processing technical field of electronic signals, and relates to the spatial remote sensing and air-to-ground observable information processing technology, in particular to the spatial synchronous technology of the space-borne bi-static SAR. On one hand, the invention broadens and receives broad beams in the azimuth direction through reducing the antenna dimension of an aircraft in the azimuth direction or only driving the partial array number of the phase array antenna of a receiving platform, thereby improving the scene length of the space-borne bi-static SAR system, on the other hand, the invention broadens and transmits the beams through reducing the antenna dimension of the aircraft in the azimuth direction or only driving the partial array number of the phase array antenna of the receiving platform, thereby improving the azimuth resolution of the space-borne bi-static SAR system. After the receiving and the transmitting beams are broadened, the scene length can achieve the magnitude of at least 1 kilometer; and the magnitude of the azimuth resolution can achieve meter level. The invention only needs to reasonably control the effective array number in the phase array antenna without changing any hardware of the prior radar system. The invention has the advantages of simple control proposal, low cost and high reliability.

Description

technical field [0001] The invention belongs to the technical field of electronic signal processing, and relates to space remote sensing and space-to-earth observation information processing technology, in particular to a star-machine bistatic SAR (Synthetic Aperture Radar, Synthetic Aperture Radar) space synchronization technology. Background technique [0002] Bistatic SAR is a synthetic aperture radar with a new system of receiving and transmitting separately. Since the receiver is always in the state of radio silence during the working process, the concealment and anti-interference ability of the SAR system are improved. By using different observation angles, various scattering information of the target can be obtained, which is beneficial to the classification and identification of the target and the improvement of the anti-stealth target capability. By providing the Doppler bandwidth from the launch platform, "forward-looking" or even "backward-looking" imaging of the...

Claims

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Application Information

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IPC IPC(8): G01S7/28G01S13/90
Inventor 皮亦鸣杨晓波曹宗杰周鹏闵锐王金峰李晋
Owner 四川电子科技大学教育发展基金会
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