A method for correcting inertial group error
An error correction and inertial group technology, which is applied in the field of synthetic aperture radar, can solve the problems of increasing sources of inertial group errors and no correction of inertial group errors.
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[0045] The present invention will be described in further detail below in conjunction with the accompanying drawings and embodiments.
[0046] see figure 1 and figure 2 As shown, the embodiment of the present invention provides an inertial error correction method for error correction of the navigation parameters of the bistatic SAR, the transmitter inertial set, and the receiver inertial set, including the following steps:
[0047] The ranging error model of bistatic SAR is established by taking the clock error of the receiver and the transmitter to be equivalent to the error in the distance;
[0048] Based on the ranging error model of bistatic SAR, the state equation of bistatic SAR ranging is established;
[0049] Establish the state equations of the receiver inertial group and the transmitter inertial group;
[0050] Establish the state equation of the cooperative navigation system based on bistatic SAR and detection target distance constraints;
[0051]Establish the ...
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