From 7f0de1440f5c83416a3cbb5b5339dc83cbe12eff Mon Sep 17 00:00:00 2001
From: Ibrahima <ibrahima.sr.sow@gmail.com>
Date: Wed, 27 Dec 2023 00:51:30 -0500
Subject: [PATCH] black reformat

---
 flight/pygnc/common/zmq_messaging.py        |  1 -
 flight/pygnc/tasks/orbit_estimator.py       | 12 +++++-------
 test/flight_pygnc/configuration/messages.py |  1 -
 3 files changed, 5 insertions(+), 9 deletions(-)

diff --git a/flight/pygnc/common/zmq_messaging.py b/flight/pygnc/common/zmq_messaging.py
index 05e00d9..c7de584 100644
--- a/flight/pygnc/common/zmq_messaging.py
+++ b/flight/pygnc/common/zmq_messaging.py
@@ -78,7 +78,6 @@ def __init__(
         self.subscriber.connect(f"tcp://localhost:{port}")
 
     def receive(self, block=True):
-
         block_flag = 0 if block else zmq.NOBLOCK
 
         try:
diff --git a/flight/pygnc/tasks/orbit_estimator.py b/flight/pygnc/tasks/orbit_estimator.py
index 895c81b..d4eb3b7 100644
--- a/flight/pygnc/tasks/orbit_estimator.py
+++ b/flight/pygnc/tasks/orbit_estimator.py
@@ -9,9 +9,10 @@
 from ..configuration import pygnc as pygnc_config
 from ..algorithms.OrbitEstimator import OrbitEKF
 
+
 def predict_orbit_ekf(orbit_ekf, prev_epoch, dt=5.0):
     orbit_ekf.predict(dt)
-    new_epoch = prev_epoch + dt # addition of seconds is defined in brahe
+    new_epoch = prev_epoch + dt  # addition of seconds is defined in brahe
     return new_epoch
 
 
@@ -28,7 +29,7 @@ def update_orbit_ekf(orbit_ekf, gps_message, prev_epoch=None):
     state_measurement_eci = brahe.frames.sECEFtoECI(
         measurement_epoch, state_measurement_ecef
     )
-    
+
     if prev_epoch is None:
         # need to initialize ekf state with first measurement
         orbit_ekf.initialize_state(state_measurement_eci)
@@ -40,7 +41,6 @@ def update_orbit_ekf(orbit_ekf, gps_message, prev_epoch=None):
     return measurement_epoch
 
 
-
 def send_orbit_estimate_message(
     pub: zmqMessagePublisher, measurement_epoch, orbit_ekf, sensor_message
 ):
@@ -68,9 +68,8 @@ def main():
     batch_data = data_parsing.unpack_batch_sensor_gps_file_to_messages_iterable(
         pygnc_config.batch_sensor_gps_filepath
     )
-    
 
-    # We predict the next state every 5 sec 
+    # We predict the next state every 5 sec
     # Every 25 sec, we process the measurement packet with an EKF update
     packet_count = 0
     prev_epoch = None
@@ -85,13 +84,12 @@ def main():
         packet_count += 1
 
         estimates.append(orbit_ekf.x)
-        for i in range(in_between_prediction_dt-1):
+        for i in range(in_between_prediction_dt - 1):
             prev_epoch = predict_orbit_ekf(orbit_ekf, prev_epoch)
             estimates.append(orbit_ekf.x)
 
     # print("Batch orbit estimation completed")
 
-
     # print("Final state estimate:")
     # print(f"\t{orbit_ekf.x}")
     # print(f"Final std dev:")
diff --git a/test/flight_pygnc/configuration/messages.py b/test/flight_pygnc/configuration/messages.py
index a572d49..725ee4d 100644
--- a/test/flight_pygnc/configuration/messages.py
+++ b/test/flight_pygnc/configuration/messages.py
@@ -7,7 +7,6 @@
 
 class TestMessagesConfiguration(unittest.TestCase):
     def test_ports_unique(self):
-
         # ensure port numbers are unique
         port_set = set()
         for message_name, message_port in message_port_dict.items():