From cd2c366e221e7cb5784f1047579bff48a0c46187 Mon Sep 17 00:00:00 2001 From: Silvan Fuhrer Date: Wed, 23 Dec 2020 10:51:17 +0100 Subject: [PATCH] AirspeedSelector: remove unnecessary reboot required and Experimental comments in params Signed-off-by: Silvan Fuhrer --- .../airspeed_selector/airspeed_selector_params.c | 16 ++++++++-------- 1 file changed, 8 insertions(+), 8 deletions(-) diff --git a/src/modules/airspeed_selector/airspeed_selector_params.c b/src/modules/airspeed_selector/airspeed_selector_params.c index ebd76852ab..7975d7fc11 100644 --- a/src/modules/airspeed_selector/airspeed_selector_params.c +++ b/src/modules/airspeed_selector/airspeed_selector_params.c @@ -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