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docs/en/advanced_config/parameter_reference.md
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@@ -25749,6 +25749,18 @@ disables trim throttle and minimum airspeed compensation based on weight.
| ------ | -------- | -------- | --------- | ------- | ---- | --------- |
| &nbsp; | | | 0.5 | -1.0 | kg | &nbsp; |
### WEIGHT_FUEL (`FLOAT`) {#WEIGHT_FUEL}
Mass of a full fuel load.
If set together with WEIGHT_BASE and WEIGHT_GROSS, the weight used for
performance scaling is reduced by the burned fuel reported in the fuel tank status.
Only a single fuel tank is supported. A zero or negative value disables fuel-based weight compensation.
| Reboot | minValue | maxValue | increment | default | unit | Read-Only |
| ------ | -------- | -------- | --------- | ------- | ---- | --------- |
| &nbsp; | | | 0.1 | -1.0 | kg | &nbsp; |
### WEIGHT_GROSS (`FLOAT`) {#WEIGHT_GROSS}
Vehicle gross weight.
@@ -25756,6 +25768,7 @@ Vehicle gross weight.
This is the actual weight of the vehicle at any time. This value will differ from WEIGHT_BASE in case weight was added
or removed from the base weight. Examples are the addition of payloads or larger batteries. A zero or negative value
disables trim throttle and minimum airspeed compensation based on weight.
If fuel-based weight compensation is enabled (WEIGHT_FUEL), set this to the takeoff weight with a full fuel load.
| Reboot | minValue | maxValue | increment | default | unit | Read-Only |
| ------ | -------- | -------- | --------- | ------- | ---- | --------- |
@@ -26299,6 +26312,27 @@ WARNING: the failures can easily cause crashes and are to be used with caution!
| ------- | -------- | -------- | --------- | ------------ | ---- | --------- |
| &check; | | | | Disabled (0) | | &nbsp; |
### SYS_FAIL_GPS_JAM (`INT32`) {#SYS_FAIL_GPS_JAM}
GPS Wrong-failure jamming state.
GNSS jamming state reported by the addressed receiver while a GPS 'wrong'
failure injection is active. The reported position is left untouched, so
'Detected' simulates a receiver that still delivers a valid fix while
reporting interference. Leave at 'Unchanged' to keep the simulated
receiver's own jamming state.
**Values:**
- `0`: Unchanged
- `1`: OK
- `2`: Mitigated
- `3`: Detected
| Reboot | minValue | maxValue | increment | default | unit | Read-Only |
| ------ | -------- | -------- | --------- | ------- | ---- | --------- |
| &nbsp; | | | | 0 | | &nbsp; |
### SYS_FAIL_GPS_WRG (`INT32`) {#SYS_FAIL_GPS_WRG}
GPS Wrong-failure fix type.
docs/en/msg_docs/TecsStatus.md
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## Fields
| Name | Type | Unit [Frame] | Range/Enum | Description |
| ------------------------------------------------------------------------- | --------- | ------------ | ---------- | -------------------------------------------------------------------------------------------------------------------- |
| <a id="fld_timestamp"></a>timestamp | `uint64` | | | time since system start (microseconds) |
| <a id="fld_altitude_sp"></a>altitude_sp | `float32` | | | Altitude setpoint AMSL [m] |
| <a id="fld_altitude_reference"></a>altitude_reference | `float32` | | | Altitude setpoint reference AMSL [m] |
| <a id="fld_altitude_time_constant"></a>altitude_time_constant | `float32` | | | Time constant of the altitude tracker [s] |
| <a id="fld_height_rate_reference"></a>height_rate_reference | `float32` | | | Height rate setpoint reference [m/s] |
| <a id="fld_height_rate_direct"></a>height_rate_direct | `float32` | | | Direct height rate setpoint from velocity reference generator [m/s] |
| <a id="fld_height_rate_setpoint"></a>height_rate_setpoint | `float32` | | | Height rate setpoint [m/s] |
| <a id="fld_height_rate"></a>height_rate | `float32` | | | Height rate [m/s] |
| <a id="fld_equivalent_airspeed_sp"></a>equivalent_airspeed_sp | `float32` | | | Equivalent airspeed setpoint [m/s] |
| <a id="fld_true_airspeed_sp"></a>true_airspeed_sp | `float32` | | | True airspeed setpoint [m/s] |
| <a id="fld_true_airspeed_filtered"></a>true_airspeed_filtered | `float32` | | | True airspeed filtered [m/s] |
| <a id="fld_true_airspeed_derivative_sp"></a>true_airspeed_derivative_sp | `float32` | | | True airspeed derivative setpoint [m/s^2] |
| <a id="fld_true_airspeed_derivative"></a>true_airspeed_derivative | `float32` | | | True airspeed derivative [m/s^2] |
| <a id="fld_true_airspeed_derivative_raw"></a>true_airspeed_derivative_raw | `float32` | | | True airspeed derivative raw [m/s^2] |
| <a id="fld_total_energy_rate_sp"></a>total_energy_rate_sp | `float32` | | | Total energy rate setpoint [m^2/s^3] |
| <a id="fld_total_energy_rate"></a>total_energy_rate | `float32` | | | Total energy rate estimate [m^2/s^3] |
| <a id="fld_total_energy_balance_rate_sp"></a>total_energy_balance_rate_sp | `float32` | | | Energy balance rate setpoint [m^2/s^3] |
| <a id="fld_total_energy_balance_rate"></a>total_energy_balance_rate | `float32` | | | Energy balance rate estimate [m^2/s^3] |
| <a id="fld_throttle_integ"></a>throttle_integ | `float32` | | | Throttle integrator value [-] |
| <a id="fld_pitch_integ"></a>pitch_integ | `float32` | | | Pitch integrator value [rad] |
| <a id="fld_throttle_sp"></a>throttle_sp | `float32` | | | Current throttle setpoint [-] |
| <a id="fld_pitch_sp_rad"></a>pitch_sp_rad | `float32` | | | Current pitch setpoint [rad] |
| <a id="fld_throttle_trim"></a>throttle_trim | `float32` | | | estimated throttle value [0,1] required to fly level at equivalent_airspeed_sp in the current atmospheric conditions |
| <a id="fld_underspeed_ratio"></a>underspeed_ratio | `float32` | | | 0: no underspeed, 1: maximal underspeed. Controller takes measures to avoid stall proportional to ratio if >0. |
| <a id="fld_fast_descend_ratio"></a>fast_descend_ratio | `float32` | | | value indicating if fast descend mode is enabled with ramp up and ramp down [0-1] |
| Name | Type | Unit [Frame] | Range/Enum | Description |
| ------------------------------------------------------------------------- | --------- | ------------ | ---------- | ------------------------------------------------------------------------------------------------------------------------ |
| <a id="fld_timestamp"></a>timestamp | `uint64` | | | time since system start (microseconds) |
| <a id="fld_altitude_sp"></a>altitude_sp | `float32` | | | Altitude setpoint AMSL [m] |
| <a id="fld_altitude_reference"></a>altitude_reference | `float32` | | | Altitude setpoint reference AMSL [m] |
| <a id="fld_altitude_time_constant"></a>altitude_time_constant | `float32` | | | Time constant of the altitude tracker [s] |
| <a id="fld_height_rate_reference"></a>height_rate_reference | `float32` | | | Height rate setpoint reference [m/s] |
| <a id="fld_height_rate_direct"></a>height_rate_direct | `float32` | | | Direct height rate setpoint from velocity reference generator [m/s] |
| <a id="fld_height_rate_setpoint"></a>height_rate_setpoint | `float32` | | | Height rate setpoint [m/s] |
| <a id="fld_height_rate"></a>height_rate | `float32` | | | Height rate [m/s] |
| <a id="fld_equivalent_airspeed_sp"></a>equivalent_airspeed_sp | `float32` | | | Equivalent airspeed setpoint [m/s] |
| <a id="fld_true_airspeed_sp"></a>true_airspeed_sp | `float32` | | | True airspeed setpoint [m/s] |
| <a id="fld_true_airspeed_filtered"></a>true_airspeed_filtered | `float32` | | | True airspeed filtered [m/s] |
| <a id="fld_true_airspeed_derivative_sp"></a>true_airspeed_derivative_sp | `float32` | | | True airspeed derivative setpoint [m/s^2] |
| <a id="fld_true_airspeed_derivative"></a>true_airspeed_derivative | `float32` | | | True airspeed derivative [m/s^2] |
| <a id="fld_true_airspeed_derivative_raw"></a>true_airspeed_derivative_raw | `float32` | | | True airspeed derivative raw [m/s^2] |
| <a id="fld_total_energy_rate_sp"></a>total_energy_rate_sp | `float32` | | | Total energy rate setpoint [m^2/s^3] |
| <a id="fld_total_energy_rate"></a>total_energy_rate | `float32` | | | Total energy rate estimate [m^2/s^3] |
| <a id="fld_total_energy_balance_rate_sp"></a>total_energy_balance_rate_sp | `float32` | | | Energy balance rate setpoint [m^2/s^3] |
| <a id="fld_total_energy_balance_rate"></a>total_energy_balance_rate | `float32` | | | Energy balance rate estimate [m^2/s^3] |
| <a id="fld_throttle_integ"></a>throttle_integ | `float32` | | | Throttle integrator value [-] |
| <a id="fld_pitch_integ"></a>pitch_integ | `float32` | | | Pitch integrator value [rad] |
| <a id="fld_throttle_sp"></a>throttle_sp | `float32` | | | Current throttle setpoint [-] |
| <a id="fld_pitch_sp_rad"></a>pitch_sp_rad | `float32` | | | Current pitch setpoint [rad] |
| <a id="fld_throttle_trim"></a>throttle_trim | `float32` | | | estimated throttle value [0,1] required to fly level at equivalent_airspeed_sp in the current atmospheric conditions |
| <a id="fld_underspeed_ratio"></a>underspeed_ratio | `float32` | | | 0: no underspeed, 1: maximal underspeed. Controller takes measures to avoid stall proportional to ratio if >0. |
| <a id="fld_fast_descend_ratio"></a>fast_descend_ratio | `float32` | | | value indicating if fast descend mode is enabled with ramp up and ramp down [0-1] |
| <a id="fld_weight_ratio"></a>weight_ratio | `float32` | | | Ratio of estimated vehicle weight to WEIGHT_BASE. Accounts for burned fuel if fuel-based weight compensation is enabled. |
## Source Message
@@ -74,6 +75,8 @@ float32 throttle_trim # estimated throttle value [0,1] required to fly level a
float32 underspeed_ratio # 0: no underspeed, 1: maximal underspeed. Controller takes measures to avoid stall proportional to ratio if >0.
float32 fast_descend_ratio # value indicating if fast descend mode is enabled with ramp up and ramp down [0-1]
float32 weight_ratio # [-] Ratio of estimated vehicle weight to WEIGHT_BASE. Accounts for burned fuel if fuel-based weight compensation is enabled.
```
:::
docs/public/config/failsafe/index.js
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docs/public/config/failsafe/index.wasm
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docs/public/config/failsafe/parameters.json
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