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removed white space noise
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@@ -246,5 +246,5 @@ fi
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#
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if param compare SYS_AUTOSTART 13001
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then
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sh /etc/init.d/13001_caipirinha_vtol
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sh /etc/init.d/13001_caipirinha_vtol
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fi
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@@ -20,7 +20,7 @@ then
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param set MC_YAWRATE_I 0.0
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param set MC_YAWRATE_D 0.0
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param set MC_YAW_FF 0.3
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#
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# Default parameters for FW
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#
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@@ -550,7 +550,7 @@ then
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sh /etc/init.d/rc.mc_apps
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fi
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fi
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#
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# VTOL setup
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#
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@@ -589,7 +589,7 @@ then
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sh /etc/init.d/rc.vtol_apps
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fi
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fi
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#
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# Start the navigator
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#
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@@ -466,7 +466,7 @@ public:
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OCTA_X,
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OCTA_PLUS,
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OCTA_COX,
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TWIN_ENGINE, /**< VTOL: one engine on each wing */
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TWIN_ENGINE, /**< VTOL: one engine on each wing */
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MAX_GEOMETRY
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};
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@@ -436,7 +436,7 @@ void VtolAttitudeControl::fill_mc_att_control_output()
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{
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_actuators_out_0.control[0] = _actuators_mc_in.control[0];
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_actuators_out_0.control[1] = _actuators_mc_in.control[1];
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_actuators_out_0.control[2] = _actuators_mc_in.control[2];
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_actuators_out_0.control[2] = _actuators_mc_in.control[2];
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_actuators_out_0.control[3] = _actuators_mc_in.control[3];
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//set neutral position for elevons
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_actuators_out_1.control[0] = _actuators_mc_in.control[2]; //roll elevon
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@@ -457,7 +457,7 @@ void VtolAttitudeControl::fill_fw_att_control_output()
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_actuators_out_1.control[0] = -_actuators_fw_in.control[0]; // roll elevon
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_actuators_out_1.control[1] = _actuators_fw_in.control[1]; // pitch elevon
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// unused now but still logged
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_actuators_out_1.control[2] = _actuators_fw_in.control[2]; // yaw
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_actuators_out_1.control[2] = _actuators_fw_in.control[2]; // yaw
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_actuators_out_1.control[3] = _actuators_fw_in.control[3]; // throttle
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}
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