Результаты (
английский) 3:
[копия]Скопировано!
Shows relevance to ensure integrity of signals (CA) in systems autonomous navigation (SAN) spacecraft (KA).For the purposes of technological independence and renewment suggested to use for this domestic system computer modeling electromagnetic compatibility.Presents the results of the analysis of circuits CA real printed circuit boards SAN KA with and without taking into account the loss, taking into account and without taking into account real-world workloads, time and frequency domain areas.For the analysis used-belted approach that is implemented in the system Talgat. Consider three illustrative examples.First, performed an evaluation of impact boundary conditions on the signal in the form of highways, taking into account and without taking into account losses in the conductors and dielectrics. Ok,That misalignment between the tracks in the beginning and in the end leads to the emergence of a large number of reflections, which can be used to override the distinctive front from the losses in real-diffuse approach.The next performed assessment of the level and cross-coupling ratio in пятипроводнои highway in time and frequency fields. Considered worst case,When the one conductor simultaneously all the rest. As a result of such evaluation revealed a high level inductive coupling, which in the middle at the end of 6.5 % on the signal level in the active line, and at the far - 2.8 %.Modeling in the frequency domain has shown that the first maximum crosstalk on the passive windows explorer is 20% of the signal in the active line, and there is the frequency, near to frequencies navigation systems.Finally, the evaluation performed synchronization signals in differential pair (JP). The difference between the signals in MT is quite large and is approximately 3.5 per cent of signal in the active windows explorer.
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