NR UE: provide velocity vector down to nr-ue.c, preparing for Doppler calculation
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@@ -569,10 +569,14 @@ typedef struct {
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// orbital angular velocity in rad/ms
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double omega;
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// satellite position at epoch time
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// satellite position vector at epoch time
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position_t pos_sat_0;
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// satellite position at 90° orbit
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// satellite position vector at 90° orbit
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position_t pos_sat_90;
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// satellite velocity vector at epoch time
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position_t vel_sat_0;
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// satellite velocity vector at 90° orbit
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position_t vel_sat_90;
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// N_common_ta_adj represents common round-trip-time between gNB and SAT received in SIB19 (ms)
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double N_common_ta_adj;
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