Remote sensing system based on satellite formation
A satellite formation and remote sensing technology, applied in the field of remote sensing, can solve the problems of inconsistency, not taking into account the antenna angle, and the beam not covering the same area, and achieve the effect of improving accuracy and time window synchronization.
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Embodiment 1
[0040] This embodiment also discloses a remote sensing imaging method, which may also be a satellite-based remote sensing imaging method, may also be a distributed synthetic aperture radar based remote sensing imaging method, or may be a satellite formation-based remote sensing imaging method method, which can be implemented by the system of the present invention and / or other alternative components. For example, a system that implements the method by using various components in the system of the present invention. In the case of no conflict or contradiction, the whole and / or part of the content of the preferred implementations of other embodiments may serve as supplements to this embodiment.
[0041] According to a preferred embodiment, the imaging method includes the main satellite 100 , the first auxiliary satellite 200 and the second auxiliary satellite 201 with the imaging sensing device 300 and the synchronization device 400 as payloads. The first auxiliary star 200 and ...
Embodiment 2
[0049] This embodiment may be a further improvement and / or supplement to Embodiment 1, and repeated content will not be repeated here. In the case of no conflict or contradiction, the whole and / or part of the content of the preferred implementations of other embodiments may serve as supplements to this embodiment.
[0050] According to a preferred embodiment, a third auxiliary star 101 with the imaging sensor device 300 and the synchronization device 400 as payloads is set outside the trajectory of the first auxiliary star 200 and the second auxiliary star 201 and flies in formation with the main star 100 . The third auxiliary star 101 is located in an adjacent orbit to the main star 100 , so that the third auxiliary star 101 forms a long-along track baseline C and a short-cut track baseline D relative to the main star 100 . The imaging sensing device 300 is based on the first spatial baseline A and the second spatial baseline B, combined with the short-cut track baseline D a...
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