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AirspeedSelector: remove unnecessary reboot required and Experimental comments in params 

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
This commit is contained in:
Silvan Fuhrer 2020-12-23 10:51:17 +01:00
parent 11dbc7e17f
commit cd2c366e22
1 changed files with 8 additions and 8 deletions
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16
src/modules/airspeed_selector/airspeed_selector_params.c
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@ -114,7 +114,6 @@ PARAM_DEFINE_INT32(ASPD_PRIMARY, 1);
*
* If set to true then the data comming from the airspeed sensors is checked for validity. Only applied if ASPD_PRIMARY > 0.
*
* @reboot_required true
* @boolean
* @group Airspeed Validator
*/
@ -129,13 +128,12 @@ PARAM_DEFINE_INT32(ASPD_DO_CHECKS, 0);
* @value 0 Disable fallback to sensor-less estimation
* @value 1 Enable fallback to sensor-less estimation
* @boolean
* @reboot_required true
* @group Airspeed Validator
*/
PARAM_DEFINE_INT32(ASPD_FALLBACK_GW, 0);
/**
* Airspeed failsafe consistency threshold (Experimental)
* Airspeed failsafe consistency threshold
*
* This specifies the minimum airspeed test ratio required to trigger a failsafe. Larger values make the check less sensitive,
* smaller values make it more sensitive. Start with a value of 1.0 when tuning. When tas_test_ratio is > 1.0 it indicates the
@ -149,7 +147,7 @@ PARAM_DEFINE_INT32(ASPD_FALLBACK_GW, 0);
PARAM_DEFINE_FLOAT(ASPD_FS_INNOV, 1.0f);
/**
* Airspeed failsafe consistency delay (Experimental)
* Airspeed failsafe consistency delay
*
* This sets the time integral of airspeed test ratio exceedance above ASPD_FS_INNOV required to trigger a failsafe.
* For example if ASPD_FS_INNOV is 1 and estimator_status.tas_test_ratio is 2.0, then the exceedance is 1.0 and the integral will
@ -163,7 +161,7 @@ PARAM_DEFINE_FLOAT(ASPD_FS_INNOV, 1.0f);
PARAM_DEFINE_FLOAT(ASPD_FS_INTEG, -1.0f);
/**
* Airspeed failsafe stop delay (Experimental)
* Airspeed failsafe stop delay
*
* Delay before stopping use of airspeed sensor if checks indicate sensor is bad.
*
@ -175,7 +173,7 @@ PARAM_DEFINE_FLOAT(ASPD_FS_INTEG, -1.0f);
PARAM_DEFINE_INT32(ASPD_FS_T1, 3);
/**
* Airspeed failsafe start delay (Experimental)
* Airspeed failsafe start delay
*
* Delay before switching back to using airspeed sensor if checks indicate sensor is good.
*
@ -187,9 +185,11 @@ PARAM_DEFINE_INT32(ASPD_FS_T1, 3);
PARAM_DEFINE_INT32(ASPD_FS_T2, 100);
/**
* Airspeed fault detection stall airspeed. (Experimental)
* Airspeed fault detection stall airspeed
*
* This is the minimum indicated airspeed at which the wing can produce 1g of lift. It is used by the airspeed sensor fault detection and failsafe calculation to detect a significant airspeed low measurement error condition and should be set based on flight test for reliable operation.
* This is the minimum indicated airspeed at which the wing can produce 1g of lift.
* It is used by the airspeed sensor fault detection and failsafe calculation to detect a
* significant airspeed low measurement error condition and should be set based on flight test for reliable operation.
*
* @group Airspeed Validator
* @unit m/s