pxmlw6n2f/Gazebo_Distributed_TCP/worlds/cessna_demo.world

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2019-03-28 10:57:49 +08:00
<?xml version="1.0" ?>
<sdf version="1.4">
<world name="default">
<gui>
<!-- A plugin for controlling the Cessna with the keyboard -->
<plugin name="cessna_keyboard" filename="libCessnaGUIPlugin.so"/>
<camera name="user_camera">
<pose>-16 0 4 0 0 0</pose>
</camera>
</gui>
<include>
<uri>model://sun</uri>
</include>
<model name="ground_plane">
<static>true</static>
<link name="link">
<collision name="collision">
<geometry>
<plane>
<normal>0 0 1</normal>
<size>5000 5000</size>
</plane>
</geometry>
<surface>
<friction>
<ode>
<mu>1</mu>
<mu2>1</mu2>
</ode>
</friction>
</surface>
</collision>
<visual name="runway">
<pose>700 0 0.1 0 0 0</pose>
<cast_shadows>false</cast_shadows>
<geometry>
<plane>
<normal>0 0 1</normal>
<size>1829 45</size>
</plane>
</geometry>
<material>
<script>
<uri>file://media/materials/scripts/gazebo.material</uri>
<name>Gazebo/Runway</name>
</script>
</material>
</visual>
<visual name="grass">
<pose>0 0 -0.1 0 0 0</pose>
<cast_shadows>false</cast_shadows>
<geometry>
<plane>
<normal>0 0 1</normal>
<size>5000 5000</size>
</plane>
</geometry>
<material>
<script>
<uri>file://media/materials/scripts/gazebo.material</uri>
<name>Gazebo/Grass</name>
</script>
</material>
</visual>
</link>
</model>
<model name="cessna_c172">
<include>
<uri>model://cessna</uri>
</include>
<link name="blade_1_visual">
<pose>1.79 0 1.350 0 0 0</pose>
<gravity>0</gravity>
</link>
<link name="wing_body_debug_visuals">
<pose>0 0 0.495 0 0 0</pose>
<gravity>0</gravity>
</link>
<!-- Plugins for controlling the thrust and control surfaces -->
<plugin name="cessna_control" filename="libCessnaPlugin.so">
<propeller>cessna_c172::propeller_joint</propeller>
<propeller_max_rpm>2500</propeller_max_rpm>
<left_aileron>cessna_c172::left_aileron_joint</left_aileron>
<left_flap>cessna_c172::left_flap_joint</left_flap>
<right_aileron>cessna_c172::right_aileron_joint</right_aileron>
<right_flap>cessna_c172::right_flap_joint</right_flap>
<elevators>cessna_c172::elevators_joint</elevators>
<rudder>cessna_c172::rudder_joint</rudder>
<propeller_p_gain>10000</propeller_p_gain>
<propeller_i_gain>0</propeller_i_gain>
<propeller_d_gain>0</propeller_d_gain>
<surfaces_p_gain>2000</surfaces_p_gain>
<surfaces_i_gain>0</surfaces_i_gain>
<surfaces_d_gain>0</surfaces_d_gain>
</plugin>
<plugin name="propeller_top_blade" filename="libLiftDragPlugin.so">
<a0>0.4</a0>
<cla>4.752798721</cla>
<cda>0.6417112299</cda>
<cma>0</cma>
<alpha_stall>1.5</alpha_stall>
<cla_stall>-3.85</cla_stall>
<cda_stall>-0.9233984055</cda_stall>
<cma_stall>0</cma_stall>
<cp>-0.37 0 0.77</cp>
<area>0.1</area>
<air_density>1.2041</air_density>
<forward>0 -1 0</forward>
<upward>1 0 0</upward>
<link_name>cessna_c172::propeller</link_name>
</plugin>
<plugin name="propeller_bottom_blade" filename="libLiftDragPlugin.so">
<a0>0.4</a0>
<cla>4.752798721</cla>
<cda>0.6417112299</cda>
<cma>0</cma>
<alpha_stall>1.5</alpha_stall>
<cla_stall>-3.85</cla_stall>
<cda_stall>-0.9233984055</cda_stall>
<cma_stall>0</cma_stall>
<cp>-0.37 0 -0.77</cp>
<area>0.1</area>
<air_density>1.2041</air_density>
<forward>0 1 0</forward>
<upward>1 0 0</upward>
<link_name>cessna_c172::propeller</link_name>
</plugin>
<plugin name="left_wing" filename="libLiftDragPlugin.so">
<a0>0.05984281113</a0>
<cla>4.752798721</cla>
<cda>0.6417112299</cda>
<cma>-1.8</cma>
<alpha_stall>0.3391428111</alpha_stall>
<cla_stall>-3.85</cla_stall>
<cda_stall>-0.9233984055</cda_stall>
<cma_stall>0</cma_stall>
<cp>-1 2.205 1.5</cp>
<area>8.08255</area>
<air_density>1.2041</air_density>
<forward>1 0 0</forward>
<upward>0 0 1</upward>
<link_name>cessna_c172::body</link_name>
<control_joint_name>cessna_c172::left_aileron_joint</control_joint_name>
<control_joint_rad_to_cl>-2.0</control_joint_rad_to_cl>
</plugin>
<plugin name="right_wing" filename="libLiftDragPlugin.so">
<a0>0.05984281113</a0>
<cla>4.752798721</cla>
<cda>0.6417112299</cda>
<cma>-1.8</cma>
<alpha_stall>0.3391428111</alpha_stall>
<cla_stall>-3.85</cla_stall>
<cda_stall>-0.9233984055</cda_stall>
<cma_stall>0</cma_stall>
<cp>-1 -2.205 1.5</cp>
<area>8.08255</area>
<air_density>1.2041</air_density>
<forward>1 0 0</forward>
<upward>0 0 1</upward>
<link_name>cessna_c172::body</link_name>
<control_joint_name>
cessna_c172::right_aileron_joint
</control_joint_name>
<control_joint_rad_to_cl>-2.0</control_joint_rad_to_cl>
</plugin>
<plugin name="elevator" filename="libLiftDragPlugin.so">
<a0>-0.2</a0>
<cla>4.752798721</cla>
<cda>0.6417112299</cda>
<cma>-1.8</cma>
<alpha_stall>0.3391428111</alpha_stall>
<cla_stall>-3.85</cla_stall>
<cda_stall>-0.9233984055</cda_stall>
<cma_stall>0</cma_stall>
<cp>-5.45 0 0.55</cp>
<area>2.03458</area>
<air_density>1.2041</air_density>
<forward>1 0 0</forward>
<upward>0 0 1</upward>
<link_name>cessna_c172::body</link_name>
<control_joint_name>cessna_c172::elevators_joint</control_joint_name>
<control_joint_rad_to_cl>-4.0</control_joint_rad_to_cl>
</plugin>
<plugin name="rudder" filename="libLiftDragPlugin.so">
<a0>0</a0>
<cla>4.752798721</cla>
<cda>0.6417112299</cda>
<cma>-1.8</cma>
<alpha_stall>0.3391428111</alpha_stall>
<cla_stall>-3.85</cla_stall>
<cda_stall>-0.9233984055</cda_stall>
<cma_stall>0</cma_stall>
<cp>-6 0 1.55</cp>
<area>1.5329</area>
<air_density>1.2041</air_density>
<forward>1 0 0</forward>
<upward>0 1 0</upward>
<link_name>cessna_c172::body</link_name>
<control_joint_name>cessna_c172::rudder_joint</control_joint_name>
<control_joint_rad_to_cl>4.0</control_joint_rad_to_cl>
</plugin>
</model>
</world>
</sdf>