beautify some identation

msg/actuator_outputs.msg

@@ -1,5 +1,5 @@
-uint64 timestamp		# time since system start (microseconds)
+uint64 timestamp				# time since system start (microseconds)
 uint8 NUM_ACTUATOR_OUTPUTS		= 16
 uint8 NUM_ACTUATOR_OUTPUT_GROUPS	= 4	# for sanity checking
 uint32 noutputs				# valid outputs
-float32[16] output			# output data, in natural output units
+float32[16] output				# output data, in natural output units

msg/airspeed.msg

@@ -1,4 +1,4 @@
-uint64 timestamp		# time since system start (microseconds)
+uint64 timestamp			# time since system start (microseconds)
 
 float32 indicated_airspeed_m_s		# indicated airspeed in m/s
 

msg/ekf2_innovations.msg

@@ -1,11 +1,11 @@
 uint64 timestamp		# time since system start (microseconds)
-float32[6] vel_pos_innov  # velocity and position innovations
-float32[3] mag_innov 	# earth magnetic field innovations
-float32 heading_innov 	# heading innovation
-float32 airspeed_innov	# airspeed innovation
-float32 beta_innov	# synthetic sideslip innovation
-float32[2] flow_innov   # flow innovation
-float32 hagl_innov      # innovation from the terrain estimator for the height above ground level measurement  (m)
+float32[6] vel_pos_innov	# velocity and position innovations
+float32[3] mag_innov 		# earth magnetic field innovations
+float32 heading_innov 		# heading innovation
+float32 airspeed_innov		# airspeed innovation
+float32 beta_innov		# synthetic sideslip innovation
+float32[2] flow_innov   	# flow innovation
+float32 hagl_innov      	# innovation from the terrain estimator for the height above ground level measurement  (m)
 float32[6] vel_pos_innov_var 	# velocity and position innovation variances
 float32[3] mag_innov_var	# earth magnetic field innovation variance
 float32 heading_innov_var 	# heading innovation variance

msg/ekf2_timestamps.msg

@@ -4,7 +4,7 @@
 # the timestamp field is the ekf2 reference time and matches the timestamp of
 # the sensor_combined topic.
 
-uint64 timestamp		# time since system start (microseconds)
+uint64 timestamp			 # time since system start (microseconds)
 
 int16 RELATIVE_TIMESTAMP_INVALID = 32767 # (0x7fff) If one of the relative timestamps
                                          # is set to this value, it means the associated sensor values did not update

msg/esc_report.msg

@@ -1,4 +1,4 @@
-uint64 timestamp		# time since system start (microseconds)
+uint64 timestamp					# time since system start (microseconds)
 uint8 esc_vendor					# Vendor of current ESC
 uint32 esc_errorcount					# Number of reported errors by ESC - if supported
 int32 esc_rpm						# Motor RPM, negative for reverse rotation [RPM] - if supported

msg/esc_status.msg

@@ -1,4 +1,4 @@
-uint64 timestamp		# time since system start (microseconds)
+uint64 timestamp					# time since system start (microseconds)
 uint8 CONNECTED_ESC_MAX = 8				# The number of ESCs supported. Current (Q2/2013) we support 8 ESCs
 
 uint8 ESC_VENDOR_GENERIC = 0				# generic ESC

msg/home_position.msg

@@ -1,6 +1,6 @@
 # GPS home position in WGS84 coordinates.
 
-uint64 timestamp		# time since system start (microseconds)
+uint64 timestamp			# time since system start (microseconds)
 
 float64 lat				# Latitude in degrees
 float64 lon				# Longitude in degrees

msg/manual_control_setpoint.msg

@@ -1,7 +1,7 @@
-uint64 timestamp		# time since system start (microseconds)
+uint64 timestamp			# time since system start (microseconds)
 
 uint8 SWITCH_POS_NONE = 0		# switch is not mapped
-uint8 SWITCH_POS_ON = 1			# switch activated (value = 1)
+uint8 SWITCH_POS_ON = 1		# switch activated (value = 1)
 uint8 SWITCH_POS_MIDDLE = 2		# middle position (value = 0)
 uint8 SWITCH_POS_OFF = 3		# switch not activated (value = -1)
 int8 MODE_SLOT_NONE = -1		# no mode slot assigned

msg/mission.msg

@@ -1,4 +1,4 @@
-uint64 timestamp		# time since system start (microseconds)
+uint64 timestamp	# time since system start (microseconds)
 uint8 dataman_id	# default 0, there are two offboard storage places in the dataman: 0 or 1
 
 uint16 count		# count of the missions stored in the dataman

msg/mission_result.msg

@@ -1,4 +1,4 @@
-uint64 timestamp		# time since system start (microseconds)
+uint64 timestamp				# time since system start (microseconds)
 uint8 MISSION_EXECUTION_MODE_NORMAL = 0	# Execute the mission according to the planned items
 uint8 MISSION_EXECUTION_MODE_REVERSE = 1	# Execute the mission in reverse order, ignoring commands and converting all waypoints to normal ones
 uint8 MISSION_EXECUTION_MODE_FAST_FORWARD = 2	# Execute the mission as fast as possible, for example converting loiter waypoints to normal ones

msg/mount_orientation.msg

@@ -1,2 +1,2 @@
-uint64 timestamp		# time since system start (microseconds)
-float32[3] attitude_euler_angle	    # Attitude/direction of the mount as euler angles in rad
+uint64 timestamp				# time since system start (microseconds)
+float32[3] attitude_euler_angle		# Attitude/direction of the mount as euler angles in rad

msg/parameter_update.msg

@@ -2,4 +2,4 @@
 
 uint64 timestamp		# time since system start (microseconds)
 
-uint32 instance       # Instance count - constantly incrementing
+uint32 instance		# Instance count - constantly incrementing

msg/position_setpoint.msg

@@ -1,6 +1,6 @@
 # this file is only used in the position_setpoint triple as a dependency
 
-uint64 timestamp	# time since system start (microseconds)
+uint64 timestamp		# time since system start (microseconds)
 
 uint8 SETPOINT_TYPE_POSITION=0	# position setpoint
 uint8 SETPOINT_TYPE_VELOCITY=1	# velocity setpoint

msg/sensor_accel.msg

@@ -1,4 +1,4 @@
-uint64 timestamp		# time since system start (microseconds)
+uint64 timestamp	# time since system start (microseconds)
 uint32 device_id	# unique device ID for the sensor that does not change between power cycles
 
 uint64 error_count

msg/sensor_combined.msg

@@ -5,9 +5,9 @@
 # change with board revisions and sensor updates.
 #
 
-uint64 timestamp		# time since system start (microseconds)
+uint64 timestamp				# time since system start (microseconds)
 
-int32 RELATIVE_TIMESTAMP_INVALID = 2147483647 # (0x7fffffff) If one of the relative timestamps is set to this value, it means the associated sensor values are invalid
+int32 RELATIVE_TIMESTAMP_INVALID = 2147483647	# (0x7fffffff) If one of the relative timestamps is set to this value, it means the associated sensor values are invalid
 
 # gyro timstamp is equal to the timestamp of the message
 float32[3] gyro_rad			# average angular rate measured in the XYZ body frame in rad/s over the last gyro sampling period

msg/ulog_stream.msg

@@ -4,14 +4,14 @@
 uint64 timestamp		# time since system start (microseconds)
 
 # flags bitmasks
-uint8 FLAGS_NEED_ACK = 1     # if set, this message requires to be acked.
-                             # Acked messages are published synchronous: a
-                             # publisher waits for an ack before sending the
-                             # next message
+uint8 FLAGS_NEED_ACK = 1	# if set, this message requires to be acked.
+				# Acked messages are published synchronous: a
+				# publisher waits for an ack before sending the
+				# next message
 
-uint8 length                 # length of data
-uint8 first_message_offset   # offset into data where first message starts. This
-                             # can be used for recovery, when a previous message got lost
-uint16 sequence              # allows determine drops
-uint8 flags                  # see FLAGS_*
-uint8[249] data              # ulog data
+uint8 length			# length of data
+uint8 first_message_offset	# offset into data where first message starts. This
+				# can be used for recovery, when a previous message got lost
+uint16 sequence		# allows determine drops
+uint8 flags			# see FLAGS_*
+uint8[249] data		# ulog data

msg/vehicle_air_data.msg

@@ -1,7 +1,7 @@
-uint64 timestamp		# time since system start (microseconds)
+uint64 timestamp			# time since system start (microseconds)
 
 float32 baro_alt_meter			# Altitude above MSL calculated from temperature compensated baro sensor data using an ISA corrected for sea level pressure SENS_BARO_QNH.
 float32 baro_temp_celcius		# Temperature in degrees celsius
 float32 baro_pressure_pa		# Absolute pressure in pascals
 
-float32 rho						# air density
+float32 rho				# air density

msg/vehicle_attitude.msg

@@ -2,11 +2,11 @@
 
 uint64 timestamp		# time since system start (microseconds)
 
-float32 rollspeed	# Bias corrected angular velocity about X body axis in rad/s
-float32 pitchspeed	# Bias corrected angular velocity about Y body axis in rad/s
-float32 yawspeed	# Bias corrected angular velocity about Z body axis in rad/s
+float32 rollspeed		# Bias corrected angular velocity about X body axis in rad/s
+float32 pitchspeed		# Bias corrected angular velocity about Y body axis in rad/s
+float32 yawspeed		# Bias corrected angular velocity about Z body axis in rad/s
 
-float32[4] q		# Quaternion rotation from NED earth frame to XYZ body frame
+float32[4] q			# Quaternion rotation from NED earth frame to XYZ body frame
 float32[4] delta_q_reset 	# Amount by which quaternion has changed during last reset
 uint8 quat_reset_counter	# Quaternion reset counter
 

msg/vehicle_attitude_setpoint.msg

@@ -2,29 +2,29 @@ uint64 timestamp		# time since system start (microseconds)
 int8 LANDING_GEAR_UP = 1	# landing gear up
 int8 LANDING_GEAR_DOWN = -1	# landing gear down
 
-float32 roll_body				# body angle in NED frame
-float32 pitch_body				# body angle in NED frame
-float32 yaw_body				# body angle in NED frame
+float32 roll_body		# body angle in NED frame
+float32 pitch_body		# body angle in NED frame
+float32 yaw_body		# body angle in NED frame
 
-float32 yaw_sp_move_rate		# rad/s (commanded by user)
+float32 yaw_sp_move_rate	# rad/s (commanded by user)
 
 # For quaternion-based attitude control
-float32[4] q_d					# Desired quaternion for quaternion control
-bool q_d_valid					# Set to true if quaternion vector is valid
+float32[4] q_d			# Desired quaternion for quaternion control
+bool q_d_valid			# Set to true if quaternion vector is valid
 
-float32 thrust					# Thrust in Newton the power system should generate
+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 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)
-bool disable_mc_yaw_control			# control yaw for mc (used for vtol weather-vane mode)
+bool fw_control_yaw		# control heading with rudder (used for auto takeoff on runway)
+bool disable_mc_yaw_control	# control yaw for mc (used for vtol weather-vane mode)
 
-uint8 apply_flaps       # flap config specifier
-uint8 FLAPS_OFF = 0     # no flaps
-uint8 FLAPS_LAND = 1    # landing config flaps
-uint8 FLAPS_TAKEOFF = 2 # take-off config flaps
+uint8 apply_flaps       	# flap config specifier
+uint8 FLAPS_OFF = 0     	# no flaps
+uint8 FLAPS_LAND = 1    	# landing config flaps
+uint8 FLAPS_TAKEOFF = 2 	# take-off config flaps
 
 float32 landing_gear
 

msg/vehicle_command.msg

@@ -1,4 +1,4 @@
-uint64 timestamp		# time since system start (microseconds)
+uint64 timestamp						# time since system start (microseconds)
 
 uint16 VEHICLE_CMD_CUSTOM_0 = 0				# test command
 uint16 VEHICLE_CMD_CUSTOM_1 = 1				# test command

msg/vehicle_constraints.msg

@@ -1,7 +1,7 @@
 # Local setpoint constraints in NED frame
 # setting something to NaN means that no limit is provided
 
-uint64 timestamp		# time since system start (microseconds)
+uint64 timestamp	# time since system start (microseconds)
 
 float32 yawspeed	# in radians/sec
 float32 speed_xy	# in meters/sec

msg/vehicle_land_detected.msg

@@ -1,6 +1,6 @@
 uint64 timestamp	# time since system start (microseconds)
 bool landed		# true if vehicle is currently landed on the ground
-bool freefall	# true if vehicle is currently in free-fall
-bool ground_contact # true if vehicle has ground contact but is not landed
-bool maybe_landed # true if the vehicle might have landed
+bool freefall		# true if vehicle is currently in free-fall
+bool ground_contact	# true if vehicle has ground contact but is not landed
+bool maybe_landed	# true if the vehicle might have landed
 float32 alt_max 	# maximum altitude in [m] that can be reached

msg/vehicle_local_position_setpoint.msg

@@ -1,16 +1,16 @@
 # Local position setpoint in NED frame
 # setting something to NaN means the state should not be controlled
 
-uint64 timestamp		# time since system start (microseconds)
+uint64 timestamp	# time since system start (microseconds)
 
-float32 x			# in meters NED
-float32 y			# in meters NED
-float32 z			# in meters NED
-float32 yaw			# in radians NED -PI..+PI
+float32 x		# in meters NED
+float32 y		# in meters NED
+float32 z		# in meters NED
+float32 yaw		# in radians NED -PI..+PI
 float32 yawspeed	# in radians/sec
-float32 vx			# in meters/sec
-float32 vy			# in meters/sec
-float32 vz			# in meters/sec
+float32 vx		# in meters/sec
+float32 vy		# in meters/sec
+float32 vz		# in meters/sec
 float32 acc_x		# in meters/(sec*sec)
 float32 acc_y		# in meters/(sec*sec)
 float32 acc_z		# in meters/(sec*sec)

msg/vehicle_rates_setpoint.msg

@@ -1,8 +1,8 @@
-uint64 timestamp		# time since system start (microseconds)
+uint64 timestamp	# time since system start (microseconds)
 
-float32 roll	    # body angular rates in NED frame
-float32 pitch	    # body angular rates in NED frame
-float32 yaw			# body angular rates in NED frame
-float32 thrust	    # thrust normalized to 0..1
+float32 roll		# body angular rates in NED frame
+float32 pitch		# body angular rates in NED frame
+float32 yaw		# body angular rates in NED frame
+float32 thrust		# thrust normalized to 0..1
 
 # TOPICS vehicle_rates_setpoint mc_virtual_rates_setpoint fw_virtual_rates_setpoint

msg/vehicle_roi.msg

@@ -1,12 +1,12 @@
 # Vehicle Region Of Interest (ROI)
 
-uint64 timestamp		# time since system start (microseconds)
+uint64 timestamp			# time since system start (microseconds)
 
-uint8 ROI_NONE = 0                         # No region of interest
-uint8 ROI_WPNEXT = 1                       # Point toward next MISSION with optional offset
-uint8 ROI_WPINDEX = 2                      # Point toward given MISSION
-uint8 ROI_LOCATION = 3                     # Point toward fixed location
-uint8 ROI_TARGET = 4                       # Point toward target
+uint8 ROI_NONE = 0			# No region of interest
+uint8 ROI_WPNEXT = 1			# Point toward next MISSION with optional offset
+uint8 ROI_WPINDEX = 2			# Point toward given MISSION
+uint8 ROI_LOCATION = 3			# Point toward fixed location
+uint8 ROI_TARGET = 4			# Point toward target
 uint8 ROI_ENUM_END = 5
 
 uint8 mode          # ROI mode (see above)

msg/vehicle_status.msg

@@ -1,6 +1,6 @@
 # If you change the order, add or remove arming_state_t states make sure to update the arrays
 # in state_machine_helper.cpp as well.
-uint64 timestamp		# time since system start (microseconds)
+uint64 timestamp				# time since system start (microseconds)
 
 uint8 ARMING_STATE_INIT = 0
 uint8 ARMING_STATE_STANDBY = 1

msg/vehicle_status_flags.msg

@@ -1,6 +1,6 @@
 # This is a struct used by the commander internally.
 
-uint64 timestamp		# time since system start (microseconds)
+uint64 timestamp				# time since system start (microseconds)
 
 bool condition_calibration_enabled
 bool condition_system_sensors_initialized

msg/vtol_vehicle_status.msg

@@ -5,10 +5,10 @@ uint8 VEHICLE_VTOL_STATE_TRANSITION_TO_MC = 2
 uint8 VEHICLE_VTOL_STATE_MC = 3
 uint8 VEHICLE_VTOL_STATE_FW = 4
 
-uint64 timestamp		# time since system start (microseconds)
+uint64 timestamp			# time since system start (microseconds)
 
 bool vtol_in_rw_mode			# true: vtol vehicle is in rotating wing mode
 bool vtol_in_trans_mode
 bool in_transition_to_fw		# True if VTOL is doing a transition from MC to FW
-bool vtol_transition_failsafe	# vtol in transition failsafe mode
+bool vtol_transition_failsafe		# vtol in transition failsafe mode
 bool fw_permanent_stab			# In fw mode stabilize attitude even if in manual mode