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tecs_status.msg: add comments to states

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Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
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Silvan Fuhrer
2023-01-26 17:04:43 +01:00
parent 5099a91f87
commit fc1c5da92c
1 changed files with 27 additions and 27 deletions
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msg/TecsStatus.msg
+27 -27
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@@ -1,4 +1,31 @@
uint64 timestamp # time since system start (microseconds)
float32 altitude_sp # Altitude setpoint AMSL [m]
float32 altitude_filtered # Altitude filtered AMSL [m]
float32 height_rate_setpoint # Height rate setpoint [m/s]
float32 height_rate # Height rate [m/s]
float32 equivalent_airspeed_sp # Equivalent airpseed setpoint [m/s]
float32 true_airspeed_sp # True airpseed setpoint [m/s]
float32 true_airspeed_filtered # True airpseed filtered [m/s]
float32 true_airspeed_derivative_sp # True airpseed derivative setpoint [m/s^2]
float32 true_airspeed_derivative # True airpseed derivative [m/s^2]
float32 true_airspeed_derivative_raw # True airpseed derivative raw [m/s^2]
float32 total_energy_rate_sp # Total energy rate setpoint [m^2/s^3]
float32 total_energy_rate # Total energy rate estimate [m^2/s^3]
float32 total_energy_balance_rate_sp # Energy balance rate setpoint [m^2/s^3]
float32 total_energy_balance_rate # Energy balance rate estimate [m^2/s^3]
float32 throttle_integ # Throttle integrator value [-]
float32 pitch_integ # Pitch integrator value [rad]
float32 throttle_sp # Current throttle setpoint [-]
float32 pitch_sp_rad # Current pitch setpoint [rad]
float32 throttle_trim # estimated throttle value [0,1] required to fly level at equivalent_airspeed_sp in the current atmospheric conditions
# TECS mode
uint8 mode
uint8 TECS_MODE_NORMAL = 0
uint8 TECS_MODE_UNDERSPEED = 1
uint8 TECS_MODE_TAKEOFF = 2
@@ -6,30 +33,3 @@ uint8 TECS_MODE_LAND = 3
uint8 TECS_MODE_LAND_THROTTLELIM = 4
uint8 TECS_MODE_BAD_DESCENT = 5
uint8 TECS_MODE_CLIMBOUT = 6
float32 altitude_sp
float32 altitude_filtered
float32 height_rate_setpoint
float32 height_rate
float32 equivalent_airspeed_sp
float32 true_airspeed_sp
float32 true_airspeed_filtered
float32 true_airspeed_derivative_sp
float32 true_airspeed_derivative
float32 true_airspeed_derivative_raw
float32 total_energy_rate
float32 total_energy_balance_rate
float32 total_energy_rate_sp
float32 total_energy_balance_rate_sp
float32 throttle_integ
float32 pitch_integ
float32 throttle_sp
float32 pitch_sp_rad
float32 throttle_trim # estimated throttle value [0,1] required to fly level at equivalent_airspeed_sp in the current atmospheric conditions
uint8 mode