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A Satellite Platform Attitude Maneuvering Method Based on Spaceborne SAR Multi-azimuth Repeated Observation

A satellite platform and attitude maneuvering technology, which is applied in the field of satellite platform attitude maneuvering, achieves the best image quality, simplifies processing difficulty, and smooth transition effects

Active Publication Date: 2021-10-01
XIAN INSTITUE OF SPACE RADIO TECH
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  • Claims
  • Application Information

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At present, there is no suitable method for solving the above problems

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  • A Satellite Platform Attitude Maneuvering Method Based on Spaceborne SAR Multi-azimuth Repeated Observation
  • A Satellite Platform Attitude Maneuvering Method Based on Spaceborne SAR Multi-azimuth Repeated Observation
  • A Satellite Platform Attitude Maneuvering Method Based on Spaceborne SAR Multi-azimuth Repeated Observation

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Embodiment Construction

[0056] The present invention will be further elaborated below in conjunction with embodiment.

[0057] The new multi-azimuth observation mode requires the satellite platform to maneuver within a large range of azimuth rotation angles to achieve multiple sliding spotlight mode imaging of military areas. Between two adjacent imagings, it is necessary to quickly maneuver the satellite platform, adjust the antenna beam pointing to the starting position of the scene again, and then start the next sliding spotlight imaging process.

[0058] attached figure 1 The working principle of multi-azimuth observation mode is given. In the stage 1 noted in the figure, the spaceborne SAR starts to perform sliding spotlight imaging of the scene in azimuth and super large oblique angle; start position and start Phase 2 of sliding beamforming imaging. And so on, until the entire star completes all n times of sliding spotlight imaging, so as to realize the multi-azimuth repeated observation of ...

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Abstract

The present invention relates to a satellite platform attitude maneuvering method for repeated multi-azimuth observations by spaceborne SAR, s1, determining the satellite platform attitude maneuvering method for the first imaging, that is, determining the position of the satellite platform at the initial imaging moment, the satellite attitude and the first imaging process the virtual rotation center in ; s2, perform sliding spotlight imaging, and determine the satellite position at the start of the next imaging; s3, determine the two adjacent The attitude of the satellite in the maneuvering process between imaging and the virtual rotation center in the next imaging process, adjust the beam pointing to the azimuth starting position of the scene during the attitude maneuvering adjustment process; s4, repeat steps s2 and s3 until the imaging work is completed; In each sliding beam spotting imaging process mentioned above, the beam center of the satellite platform always points to the virtual rotation center determined in each imaging process.

Description

technical field [0001] The invention belongs to the technical field of space microwave remote sensing, and in particular relates to a satellite platform attitude maneuvering method. Background technique [0002] In order to improve the reconnaissance effectiveness of spaceborne SAR, it is necessary to have the ability to repeatedly observe military sensitive areas in multiple azimuths during a single transit. If it is realized by using the phased array antenna system, it realizes beam scanning and repeated observation by controlling the phase-shift code of the receiving and transmitting channels. The advantage of this method is that the satellite platform does not need to maneuver, but the disadvantage is that the antenna beam gain will increase with the rotation angle. big and low. This will lead to the loss of echo signal-to-noise ratio and the sharp deterioration of SAR image quality. If the reflector antenna is used to realize it, it needs to be realized by maneuvering...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01S13/90G01S7/02H01Q3/02H01Q1/28
CPCG01S7/02G01S13/90H01Q1/288H01Q3/02
Inventor 冯帆贺荣荣雷少敏孙嘉金阿鑫侯若涵杨娟娟党红杏
Owner XIAN INSTITUE OF SPACE RADIO TECH
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