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AirspeedSelector: remove unnecessary reboot required and Experimental comments in params

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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. * 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 * @boolean
* @group Airspeed Validator * @group Airspeed Validator
*/ */
@@ -129,13 +128,12 @@ PARAM_DEFINE_INT32(ASPD_DO_CHECKS, 0);
* @value 0 Disable fallback to sensor-less estimation * @value 0 Disable fallback to sensor-less estimation
* @value 1 Enable fallback to sensor-less estimation * @value 1 Enable fallback to sensor-less estimation
* @boolean * @boolean
* @reboot_required true
* @group Airspeed Validator * @group Airspeed Validator
*/ */
PARAM_DEFINE_INT32(ASPD_FALLBACK_GW, 0); 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, * 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 * 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); 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. * 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 * 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); 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. * 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); 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. * 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); 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 * @group Airspeed Validator
* @unit m/s * @unit m/s