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split takeoff into 2 phases, reseting integrators when still on runway

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Andreas Antener
2015-11-17 22:28:08 +01:00
committed by Roman
parent 0c875dd6d1
commit e987082292
6 changed files with 43 additions and 18 deletions
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msg/vehicle_attitude_setpoint.msg
+1 -1
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@@ -22,4 +22,4 @@ bool roll_reset_integral # Reset roll integral part (navigation logic change)
bool pitch_reset_integral # Reset pitch integral part (navigation logic change)
bool yaw_reset_integral # Reset yaw integral part (navigation logic change)
bool fw_control_wheel # control heading with rudder (used for auto takeoff on runway)
bool fw_control_yaw # control heading with rudder (used for auto takeoff on runway)