Plane: log quadplane transision state

ArduPlane/Log.cpp

@@ -375,8 +375,9 @@ const struct LogStructure Plane::log_structure[] = {
 // @Field: CRt: climb rate
 // @Field: TMix: transition throttle mix value
 // @Field: Sscl: speed scalar for tailsitter control surfaces
+// @Field: Trans: Transistion state
     { LOG_QTUN_MSG, sizeof(QuadPlane::log_QControl_Tuning),
-      "QTUN", "Qffffffeccff", "TimeUS,ThI,ABst,ThO,ThH,DAlt,Alt,BAlt,DCRt,CRt,TMix,Sscl", "s----mmmnn--", "F----00000-0" },
+      "QTUN", "QffffffeccffB", "TimeUS,ThI,ABst,ThO,ThH,DAlt,Alt,BAlt,DCRt,CRt,TMix,Sscl,Trans", "s----mmmnn---", "F----00000-0-" },
 
 // @LoggerMessage: AOA
 // @Description: Angle of attack and Side Slip Angle values

ArduPlane/quadplane.cpp

@@ -2941,6 +2941,7 @@ void QuadPlane::Log_Write_QControl_Tuning()
         climb_rate          : int16_t(inertial_nav.get_velocity_z()),
         throttle_mix        : attitude_control->get_throttle_mix(),
         speed_scaler        : last_spd_scaler,
+        transition_state    : static_cast<uint8_t>(transition_state)
     };
     plane.logger.WriteBlock(&pkt, sizeof(pkt));
 

ArduPlane/quadplane.h

@@ -159,6 +159,7 @@ public:
         int16_t  climb_rate;
         float    throttle_mix;
         float    speed_scaler;
+        uint8_t  transition_state;
     };
 
     MAV_TYPE get_mav_type(void) const;