From 20ec727d9fdbec46be75d21a838fef9e1c20cb88 Mon Sep 17 00:00:00 2001 From: tumbili Date: Thu, 10 Sep 2015 14:22:00 +0200 Subject: [PATCH] added option for direct yaw control with rudder for fixed wing --- msg/vehicle_attitude_setpoint.msg | 2 ++ 1 file changed, 2 insertions(+) diff --git a/msg/vehicle_attitude_setpoint.msg b/msg/vehicle_attitude_setpoint.msg index 7bbb670b31..3bbb5efa7b 100644 --- a/msg/vehicle_attitude_setpoint.msg +++ b/msg/vehicle_attitude_setpoint.msg @@ -21,3 +21,5 @@ float32 thrust # Thrust in Newton the power system should generate 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_yaw # control heading with rudder (used for auto takeoff on runway)