Space arbitrary configuration distributed SAR moving target parameter estimation method based on cancellation accumulation space-time spectrum
A technology of arbitrary configuration and parameter estimation, applied in the direction of reflection/re-radiation of radio waves, utilization of re-radiation, measurement devices, etc., can solve the problems of waste of information, large influence of signal-to-noise ratio, etc., and achieve cost savings and strong anti-noise. , to solve the effect of strong correlation signals
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specific Embodiment approach 1
[0021] Specific implementation mode 1. Combination figure 1 In this embodiment, the method for estimating the parameters of a distributed SAR moving target with any spatial configuration by using the destructive accumulation space-time spectrum, the specific process is as follows:
[0022] Step 1. According to the ultra-sparse distribution and high-speed flight characteristics of the space-borne distributed SAR, an extended space-time model of the distributed synthetic aperture radar echo signal with an arbitrary configuration in space is established;
[0023]Step 2, using the conjugate of the extended space-time model obtained in step 1 as the cancellation factor, using the method of space-time accumulation to establish an objective function, the meaning of the objective function is as follows: the cancellation factor containing the motion parameter search value Multiply with the echo signal, when the phase of the slow-time sampling point corresponding to the cancellation fac...
specific Embodiment approach 2
[0025] Embodiment 2. This embodiment is a further description of Embodiment 1. The specific process of Step 1 is as follows:
[0026] Step 11. Use the signal transmitting satellite as the reference star, and the small satellites in the formation only receive the echo signal. With the sub-satellite point of the reference star as the origin, establish a three-dimensional rectangular coordinate system, where the X axis is along the course, and the Y axis is parallel to the ground. The heading is inscribed in the horizontal plane of , and the Z axis is perpendicular to the ground;
[0027] Step 12. At t=0, the reference star is the reference array element, and the coordinates of the reference array element are (0, 0, H), where H is the height of the reference array element from the ground, and the coordinates of the nth array element are ( B an , B rn , H+B vn ), wherein, n=1, 2, ..., N, N is the number of array elements, that is, the number of formation small satellites; the c...
specific Embodiment approach 3
[0049] Specific embodiment 3. This embodiment is a further description of step 2 in specific embodiment 1 or 2. The objective function described in step 2 is expressed as:
[0050]
[0051]
[0052] in, is the cancellation factor of the kth slow moment of the nth array element, for complex conjugate transpose, It is the kth pulse of the nth array element, the azimuth direction signal of a certain range unit containing the target on the range ring.
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