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params: make parameter units more consistent (#15502)
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@@ -587,7 +587,7 @@ PARAM_DEFINE_FLOAT(COM_ARM_EKF_GB, 0.0011f);
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* Maximum accelerometer inconsistency between IMU units that will allow arming
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*
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* @group Commander
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* @unit m/s/s
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* @unit m/s^2
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* @min 0.1
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* @max 1.0
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* @decimal 2
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@@ -703,7 +703,7 @@ PARAM_DEFINE_INT32(COM_ARM_AUTH_REQ, 0);
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* This sets number of seconds that the position checks need to be failed before the failsafe will activate.
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* The default value has been optimised for rotary wing applications. For fixed wing applications, a larger value between 5 and 10 should be used.
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*
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* @unit sec
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* @unit s
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* @reboot_required true
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* @group Commander
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* @min 1
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@@ -720,7 +720,7 @@ PARAM_DEFINE_INT32(COM_POS_FS_DELAY, 1);
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* If position checks are failing, the probation delay will increase by COM_POS_FS_GAIN seconds for every lapsed second up to a maximum of 100 seconds.
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* The default value has been optimised for rotary wing applications. For fixed wing applications, a value of 1 should be used.
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*
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* @unit sec
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* @unit s
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* @reboot_required true
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* @group Commander
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* @min 1
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@@ -55,7 +55,7 @@
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*
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* @min 60
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* @max 180
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* @unit degrees
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* @unit deg
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* @group Failure Detector
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*/
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PARAM_DEFINE_INT32(FD_FAIL_R, 60);
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@@ -73,7 +73,7 @@ PARAM_DEFINE_INT32(FD_FAIL_R, 60);
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*
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* @min 60
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* @max 180
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* @unit degrees
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* @unit deg
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* @group Failure Detector
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*/
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PARAM_DEFINE_INT32(FD_FAIL_P, 60);
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@@ -123,7 +123,7 @@ PARAM_DEFINE_INT32(FD_EXT_ATS_EN, 0);
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*
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* External ATS is required by ASTM F3322-18.
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*
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* @unit microseconds
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* @unit us
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* @decimal 2
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*
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* @group Failure Detector
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