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https://github.com/PX4/PX4-Autopilot.git
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0c835dcc17
Add a WEIGHT_FUEL parameter for the mass of a full fuel load. When set, the weight used for trim throttle, min/stall airspeed, and climb/sink rate scaling is reduced by the burned fuel mass derived from fuel_tank_status (filtered to reject sloshing). Disabled by default.
34 lines
1.9 KiB
Plaintext
34 lines
1.9 KiB
Plaintext
uint64 timestamp # time since system start (microseconds)
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float32 altitude_sp # Altitude setpoint AMSL [m]
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float32 altitude_reference # Altitude setpoint reference AMSL [m]
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float32 altitude_time_constant # Time constant of the altitude tracker [s]
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float32 height_rate_reference # Height rate setpoint reference [m/s]
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float32 height_rate_direct # Direct height rate setpoint from velocity reference generator [m/s]
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float32 height_rate_setpoint # Height rate setpoint [m/s]
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float32 height_rate # Height rate [m/s]
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float32 equivalent_airspeed_sp # Equivalent airspeed setpoint [m/s]
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float32 true_airspeed_sp # True airspeed setpoint [m/s]
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float32 true_airspeed_filtered # True airspeed filtered [m/s]
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float32 true_airspeed_derivative_sp # True airspeed derivative setpoint [m/s^2]
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float32 true_airspeed_derivative # True airspeed derivative [m/s^2]
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float32 true_airspeed_derivative_raw # True airspeed derivative raw [m/s^2]
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float32 total_energy_rate_sp # Total energy rate setpoint [m^2/s^3]
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float32 total_energy_rate # Total energy rate estimate [m^2/s^3]
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float32 total_energy_balance_rate_sp # Energy balance rate setpoint [m^2/s^3]
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float32 total_energy_balance_rate # Energy balance rate estimate [m^2/s^3]
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float32 throttle_integ # Throttle integrator value [-]
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float32 pitch_integ # Pitch integrator value [rad]
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float32 throttle_sp # Current throttle setpoint [-]
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float32 pitch_sp_rad # Current pitch setpoint [rad]
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float32 throttle_trim # estimated throttle value [0,1] required to fly level at equivalent_airspeed_sp in the current atmospheric conditions
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float32 underspeed_ratio # 0: no underspeed, 1: maximal underspeed. Controller takes measures to avoid stall proportional to ratio if >0.
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float32 fast_descend_ratio # value indicating if fast descend mode is enabled with ramp up and ramp down [0-1]
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float32 weight_ratio # [-] Ratio of estimated vehicle weight to WEIGHT_BASE. Accounts for burned fuel if fuel-based weight compensation is enabled.
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