Method for estimating fussy component space angle and ambiguity-resolving multi-channel SAR (segmentation and resassembly sublayer) orientation
A space angle and component technology, applied in the field of airborne multi-channel SAR wide scene surveying and mapping, can solve the problems of target steering vector mismatch, estimated signal cancellation, etc.
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[0080] The technical scheme of the present invention is described in detail below in conjunction with accompanying drawing:
[0081] Airborne radar geometry such as figure 1 As shown, the carrier aircraft flies along the X-axis at the speed V, and the flight height of the carrier aircraft is H. M uniform linear arrays are distributed along the straight line of the course, and the leftmost array element along the navigation direction is stipulated as the transceiver array element ( figure 1 The middle is array element 1), and the rest are receiving array elements. Assuming that the aircraft is above the coordinate origin at t=0, at a certain time t, the position of the aircraft is x=V*t, then the slant distance from the target to the mth array element is:
[0082] R m 2 (t)=R 0 2 +(x+(m-1)d) 2 m=1,...,N
[0083] = R 0 2 +(V t+(m-1)d) 2
[0084] where R 0 2 =H 2 +y 0 2 , H represents the height of the aircraft, and d represents the array element spacin...
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