fix small

s2e-ff/data/initialize_files/components/relative_attitude_sensor.ini

@@ -8,39 +8,5 @@ target_sat_id = 1
 // When this value is negative, reference_sat_id is automatically set as the mounting satellite ID
 reference_sat_id = -1
 
-[SENSOR_BASE_RELATIVE_ATTITUDE_SENSOR]
-// The coordinate of the error is selected by the error_frame
-// Scale factor [-]
-scale_factor_c(0) = 1;
-scale_factor_c(1) = 0;
-scale_factor_c(2) = 0;
-scale_factor_c(3) = 0;
-scale_factor_c(4) = 1;
-scale_factor_c(5) = 0;
-scale_factor_c(6) = 0;
-scale_factor_c(7) = 0;
-scale_factor_c(8) = 1;
-
-// Constant bias noise [rad]
-constant_bias_c_rad(0) = 0.0
-constant_bias_c_rad(1) = 0.0
-constant_bias_c_rad(2) = 0.0
-
-// Standard deviation of normal random noise [rad]
-normal_random_standard_deviation_c_rad(0) = 0.0
-normal_random_standard_deviation_c_rad(1) = 0.0
-normal_random_standard_deviation_c_rad(2) = 0.0
-
-// Standard deviation for random walk noise [rad]
-random_walk_standard_deviation_c_rad(0) = 0.0
-random_walk_standard_deviation_c_rad(1) = 0.0
-random_walk_standard_deviation_c_rad(2) = 0.0
-
-// Limit of random walk noise [rad]
-random_walk_limit_c_rad(0) = 0.0
-random_walk_limit_c_rad(1) = 0.0
-random_walk_limit_c_rad(2) = 0.0
-
-// Range [rad]
-range_to_constant_rad = 6.283186  // smaller than range_to_zero_rad
-range_to_zero_rad = 7.0
+// Standard deviation of force direction error [deg]
+error_angle_standard_deviation_deg = 1.0

s2e-ff/src/components/aocs/relative_attitude_sensor.cpp

@@ -10,7 +10,12 @@
 
 RelativeAttitudeSensor::RelativeAttitudeSensor(const int prescaler, ClockGenerator* clock_gen, Sensor& sensor_base, const int target_sat_id,
                                                const int reference_sat_id, const RelativeInformation& rel_info, const double standard_deviation_rad)
-    : Component(prescaler, clock_gen), Sensor(sensor_base), target_sat_id_(target_sat_id), reference_sat_id_(reference_sat_id), rel_info_(rel_info) {
+    : Component(prescaler, clock_gen),
+      Sensor(sensor_base),
+      target_sat_id_(target_sat_id),
+      reference_sat_id_(reference_sat_id),
+      rel_info_(rel_info),
+      angle_noise_(0.0, standard_deviation_rad) {
   direction_noise_.SetParameters(0.0, 1.0);
 }