Fix formatting for apply_channelmod.c

radio/rfsimulator/apply_channelmod.c

@@ -21,7 +21,6 @@
  *      contact@openairinterface.org
  */
 
-
 #include <complex.h>
 #include <common/utils/LOG/log.h>
 #include <openair1/SIMULATION/TOOLS/sim.h>
@@ -53,11 +52,14 @@ void rxAddInput(const c16_t *input_sig,
 {
   static uint64_t last_TS = 0;
 
-  if ((channelDesc->sat_height > 0) && (channelDesc->enable_dynamic_delay || channelDesc->enable_dynamic_Doppler)) { // model for transparent satellite on circular orbit
+  if ((channelDesc->sat_height > 0)
+      && (channelDesc->enable_dynamic_delay
+          || channelDesc->enable_dynamic_Doppler)) { // model for transparent satellite on circular orbit
     /* assumptions:
        - The Earth is spherical, the ground station is static, and that the Earth does not rotate.
        - An access or link is possible from the satellite to the ground station at all times.
-       - The ground station is located at the North Pole (positive Zaxis), and the satellite starts from the initial elevation angle 0° in the second quadrant of the YZplane.
+       - The ground station is located at the North Pole (positive Zaxis), and the satellite starts from the initial elevation angle
+       0° in the second quadrant of the YZplane.
        - Satellite moves in the clockwise direction in its circular orbit.
     */
     const double radius_earth = 6377900; // m
@@ -159,7 +161,15 @@ void rxAddInput(const c16_t *input_sig,
 
       if (TS - last_TS >= channelDesc->sampling_rate) {
         last_TS = TS;
-        LOG_I(HW, "Satellite orbit: time %f s, Position = (%f, %f, %f), Velocity = (%f, %f, %f)\n", t, pos_sat_x, pos_sat_y, pos_sat_z, vel_sat_x, vel_sat_y, vel_sat_z);
+        LOG_I(HW,
+              "Satellite orbit: time %f s, Position = (%f, %f, %f), Velocity = (%f, %f, %f)\n",
+              t,
+              pos_sat_x,
+              pos_sat_y,
+              pos_sat_z,
+              vel_sat_x,
+              vel_sat_y,
+              vel_sat_z);
         LOG_I(HW, "Uplink delay %f ms, Doppler shift UE->SAT %f kHz\n", prop_delay * 1000, f_Doppler_shift_ue_sat / 1000);
         LOG_I(HW, "Satellite velocity towards gNB: %f m/s, acceleration towards gNB: %f m/s²\n", -vel_sat_gnb, acc_sat_gnb);
       }
@@ -218,7 +228,15 @@ void rxAddInput(const c16_t *input_sig,
 
       if (TS - last_TS >= channelDesc->sampling_rate) {
         last_TS = TS;
-        LOG_I(HW, "Satellite orbit: time %f s, Position = (%f, %f, %f), Velocity = (%f, %f, %f)\n", t, pos_sat_x, pos_sat_y, pos_sat_z, vel_sat_x, vel_sat_y, vel_sat_z);
+        LOG_I(HW,
+              "Satellite orbit: time %f s, Position = (%f, %f, %f), Velocity = (%f, %f, %f)\n",
+              t,
+              pos_sat_x,
+              pos_sat_y,
+              pos_sat_z,
+              vel_sat_x,
+              vel_sat_y,
+              vel_sat_z);
         LOG_I(HW, "Downlink delay %f ms, Doppler shift SAT->UE %f kHz\n", prop_delay * 1000, f_Doppler_shift_sat_ue / 1000);
       }
     }
@@ -281,10 +299,10 @@ void rxAddInput(const c16_t *input_sig,
 
   if ((TS * nbTx) % CirSize + nbSamples <= CirSize)
     // Cast to a wrong type for compatibility !
-    LOG_D(HW,"Input power %f, output power: %f, channel path loss %f, noise coeff: %f \n",
+    LOG_D(HW,
+          "Input power %f, output power: %f, channel path loss %f, noise coeff: %f \n",
           10 * log10((double)signal_energy((int32_t *)&input_sig[(TS * nbTx) % CirSize], nbSamples)),
           10 * log10((double)signal_energy((int32_t *)after_channel_sig, nbSamples)),
           channelDesc->path_loss_dB,
           10 * log10(noise_per_sample));
 }
-

radio/rfsimulator/rfsimulator.h

@@ -31,7 +31,6 @@ void rxAddInput( const c16_t *input_sig,
                 int nbSamples,
                 uint64_t TS,
                 uint32_t CirSize,
-                 bool apply_noise
+                bool apply_noise);
-               );
 
 #endif