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vtol: correct/improve quad-chute param description 

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
This commit is contained in:
Silvan Fuhrer 2023-03-22 10:14:42 +01:00
parent 937d27f8ee
commit e58d33284a
1 changed files with 8 additions and 7 deletions
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15
src/modules/vtol_att_control/vtol_att_control_params.c
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@ -91,7 +91,7 @@ PARAM_DEFINE_FLOAT(VT_F_TRANS_DUR, 5.0f);
PARAM_DEFINE_FLOAT(VT_B_TRANS_DUR, 4.0f);
/**
* Target throttle value for the transition to fixed wing flight.
* Target throttle value for the transition to fixed-wing flight.
*
* standard vtol: pusher
*
@ -194,10 +194,11 @@ PARAM_DEFINE_FLOAT(VT_TRANS_TIMEOUT, 15.0f);
PARAM_DEFINE_FLOAT(VT_TRANS_MIN_TM, 2.0f);
/**
* QuadChute Altitude
* Quad-chute altitude
*
* Minimum altitude for fixed wing flight, when in fixed wing the altitude drops below this altitude
* the vehicle will transition back to MC mode and enter failsafe RTL
* Minimum altitude for fixed-wing flight. When the vehicle is in fixed-wing mode
* and the altitude drops below this altitude (relative altitude above local origin),
* it will instantly switch back to MC mode and execute behavior defined in COM_QC_ACT.
*
* @unit m
* @min 0.0
@ -276,8 +277,8 @@ PARAM_DEFINE_INT32(VT_FW_QC_R, 0);
/**
* Quad-chute maximum height
*
* Maximum height above the ground (if available, otherwhise above
* home if available, otherwise above the local origin) where triggering a quadchute is possible.
* Maximum height above the ground (if available, otherwise above
* Home if available, otherwise above the local origin) where triggering a quad-chute is possible.
* At high altitudes there is a big risk to deplete the battery and therefore crash if quad-chuting there.
*
* @unit m
@ -288,7 +289,7 @@ PARAM_DEFINE_INT32(VT_FW_QC_R, 0);
PARAM_DEFINE_INT32(VT_FW_QC_HMAX, 0);
/**
* Airspeed less front transition time (open loop)
* Airspeed-less front transition time (open loop)
*
* The duration of the front transition when there is no airspeed feedback available.
*