onboard/config/drone10/drone10_onboard_com.launch.py

+"""
+File: drone10_onboard_com.launch.py
+Project: Compute Max Thrust
+File Created: Monday, 13th November 2023 11:51:01 AM
+Author: LS2N-Drone
+Email: ls2n-drone@ls2n.fr
+Version: 1.0
+-----
+Brief: THIS FILE IS AUTOGENERATED DO NOT MODIFY
+-----
+Copyright ©2023 LS2N-Drone
+"""
+from launch_ros.actions import Node
+
+from launch import LaunchDescription
+
+com_node = [
+    Node(
+        package="micro_ros_agent",
+        executable="micro_ros_agent",
+        name="micro_ros_agent",
+        arguments=["udp4", "-p", "8888"],
+    )
+]
+
+
+def generate_launch_description():
+    return LaunchDescription(com_node)
\ No newline at end of file

onboard/config/drone10/drone10_onboard_params.yaml

+#
+# File: drone10_onboard_params.yaml
+# Project: Compute Max Thrust
+# File Created: Monday, 13th November 2023 11:51:01 AM
+# Author: LS2N Drone
+# Email: ls2n-drone@ls2n.fr
+# Version: 1.0
+# -----
+# Brief: THIS FILE IS AUTOGENERATED DO NOT MODIFY
+# -----
+# Copyright ©2023 LS2N-Drone
+#
+drone_bridge:
+  ros__parameters:
+    firmware: "PX4"
+    mass: 1.311
+    max_thrust: 27.431028121509364
+
+    # Max thrust can be a linear function of the battery voltage (V): max_thrust = a * V + b
+    use_battery_for_thrust: true
+    max_thrust_a: 6.680446680431132
+    max_thrust_b: -48.071124006168695
+
+    # Position/velocity PID gains
+    kp_position: 5.0
+    kd_position: 3.0
+    ki_position: 0.0
+    kp_velocity: 5.0
+    ki_velocity: 2.0
+
+    take_off_height: 1.0
\ No newline at end of file

onboard/config/drone5/drone5_onboard_com.launch.py

+"""
+File: drone5_onboard_com.launch.py
+Project: Compute Max Thrust
+File Created: Thursday, 23rd November 2023 12:08:17 PM
+Author: LS2N-Drone
+Email: ls2n-drone@ls2n.fr
+Version: 1.0
+-----
+Brief: THIS FILE IS AUTOGENERATED DO NOT MODIFY
+-----
+Copyright ©2023 LS2N-Drone
+"""
+from launch_ros.actions import Node
+
+from launch import LaunchDescription
+
+com_node = [
+    Node(
+        package="micro_ros_agent",
+        executable="micro_ros_agent",
+        name="micro_ros_agent",
+        arguments=["udp4", "-p", "8888"],
+    )
+]
+
+
+def generate_launch_description():
+    return LaunchDescription(com_node)
\ No newline at end of file

onboard/config/drone5/drone5_onboard_params.yaml

+#
+# File: drone5_onboard_params.yaml
+# Project: Compute Max Thrust
+# File Created: Thursday, 23rd November 2023 12:08:17 PM
+# Author: LS2N Drone
+# Email: ls2n-drone@ls2n.fr
+# Version: 1.0
+# -----
+# Brief: THIS FILE IS AUTOGENERATED DO NOT MODIFY
+# -----
+# Copyright ©2023 LS2N-Drone
+#
+drone_bridge:
+  ros__parameters:
+    firmware: "PX4"
+    mass: 1.214
+    max_thrust: 49.71450590144474
+
+    # Max thrust can be a linear function of the battery voltage (V): max_thrust = a * V + b
+    use_battery_for_thrust: true
+    max_thrust_a: 10.464503970421976
+    max_thrust_b: -67.35860955446397
+
+    # Position/velocity PID gains
+    kp_position: 5.0
+    kd_position: 3.0
+    ki_position: 0.0
+    kp_velocity: 5.0
+    ki_velocity: 2.0
+
+    take_off_height: 1.0
\ No newline at end of file

onboard/config/drone6/drone6_onboard_com.launch.py

+"""
+File: drone6_onboard_com.launch.py
+Project: Compute Max Thrust
+File Created: Thursday, 23rd November 2023 10:31:03 AM
+Author: LS2N-Drone
+Email: ls2n-drone@ls2n.fr
+Version: 1.0
+-----
+Brief: THIS FILE IS AUTOGENERATED DO NOT MODIFY
+-----
+Copyright ©2023 LS2N-Drone
+"""
+from launch_ros.actions import Node
+
+from launch import LaunchDescription
+
+com_node = [
+    Node(
+        package="micro_ros_agent",
+        executable="micro_ros_agent",
+        name="micro_ros_agent",
+        arguments=["udp4", "-p", "8888"],
+    )
+]
+
+
+def generate_launch_description():
+    return LaunchDescription(com_node)
\ No newline at end of file

onboard/config/drone6/drone6_onboard_params.yaml

+#
+# File: drone6_onboard_params.yaml
+# Project: Compute Max Thrust
+# File Created: Thursday, 23rd November 2023 10:31:03 AM
+# Author: LS2N Drone
+# Email: ls2n-drone@ls2n.fr
+# Version: 1.0
+# -----
+# Brief: THIS FILE IS AUTOGENERATED DO NOT MODIFY
+# -----
+# Copyright ©2023 LS2N-Drone
+#
+drone_bridge:
+  ros__parameters:
+    firmware: "PX4"
+    mass: 1.23
+    max_thrust: 50.84493960530867
+
+    # Max thrust can be a linear function of the battery voltage (V): max_thrust = a * V + b
+    use_battery_for_thrust: true
+    max_thrust_a: 10.46436604403289
+    max_thrust_b: -67.41745247480557
+
+    # Position/velocity PID gains
+    kp_position: 5.0
+    kd_position: 3.0
+    ki_position: 0.0
+    kp_velocity: 5.0
+    ki_velocity: 2.0
+
+    take_off_height: 1.0
\ No newline at end of file

onboard/config/drone7/drone7_onboard_com.launch.py

+"""
+File: drone7_onboard_com.launch.py
+Project: Compute Max Thrust
+File Created: Wednesday, 22nd November 2023 15:03:29 PM
+Author: LS2N-Drone
+Email: ls2n-drone@ls2n.fr
+Version: 1.0
+-----
+Brief: THIS FILE IS AUTOGENERATED DO NOT MODIFY
+-----
+Copyright ©2023 LS2N-Drone
+"""
+from launch_ros.actions import Node
+
+from launch import LaunchDescription
+
+com_node = [
+    Node(
+        package="micro_ros_agent",
+        executable="micro_ros_agent",
+        name="micro_ros_agent",
+        arguments=["udp4", "-p", "8888"],
+    )
+]
+
+
+def generate_launch_description():
+    return LaunchDescription(com_node)
\ No newline at end of file

onboard/config/drone7/drone7_onboard_params.yaml

+#
+# File: drone7_onboard_params.yaml
+# Project: Compute Max Thrust
+# File Created: Wednesday, 22nd November 2023 15:03:29 PM
+# Author: LS2N Drone
+# Email: ls2n-drone@ls2n.fr
+# Version: 1.0
+# -----
+# Brief: THIS FILE IS AUTOGENERATED DO NOT MODIFY
+# -----
+# Copyright ©2023 LS2N-Drone
+#
+drone_bridge:
+  ros__parameters:
+    firmware: "PX4"
+    mass: 1.239
+    max_thrust: 58.20951868670538
+
+    # Max thrust can be a linear function of the battery voltage (V): max_thrust = a * V + b
+    use_battery_for_thrust: true
+    max_thrust_a: 12.548426909355635
+    max_thrust_b: -84.62102178896514
+
+    # Position/velocity PID gains
+    kp_position: 5.0
+    kd_position: 3.0
+    ki_position: 0.0
+    kp_velocity: 5.0
+    ki_velocity: 2.0
+
+    take_off_height: 1.0
\ No newline at end of file