High-dynamic satellite navigation receiver performance evaluating method
A satellite navigation and receiver technology, applied in satellite radio beacon positioning systems, measuring devices, instruments, etc., can solve the problems of high time cost and labor cost, cumbersome test preparation work, and insufficient test coverage, etc., to make up for the infinite Defects in standard data, shortening the time for test preparation, and solving the effects of insufficient coverage
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[0019] A method for evaluating the performance of a highly dynamic satellite navigation receiver, the steps of which are:
[0020] 1. Full motion scene editing
[0021] According to the dynamic range of the receiver, write the dynamic test scene in the earth coordinate system according to the aircraft motion model. The aircraft motion model is as follows:
[0022] (1)
[0023] In the formula: ——scene simulation step size;
[0024] , ——the jerk of the aircraft at the i-th step, and at the i-1 step;
[0025] , ——the acceleration of the aircraft at the i-th step, the i-1 step;
[0026] , ——the speed of the aircraft at the i-th step, the i-1 step;
[0027] , ——The position of the aircraft at the i-th step, the i-1 step.
[0028] In a full-motion scene, the jerk, acceleration, and velocity timing diagrams are as follows: figure 1 , while satisfying the following relationship:
[0029] (2)
[0030] In the formula: ——respectively, jerk forward maxim...
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