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vtol: correct/improve quad-chute param description

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Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
This commit is contained in:
Silvan Fuhrer
2023-03-24 13:33:52 +01:00
parent 937d27f8ee
commit e58d33284a
1 changed files with 8 additions and 7 deletions
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src/modules/vtol_att_control/vtol_att_control_params.c
+8 -7
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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); 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 * standard vtol: pusher
* *
@@ -194,10 +194,11 @@ PARAM_DEFINE_FLOAT(VT_TRANS_TIMEOUT, 15.0f);
PARAM_DEFINE_FLOAT(VT_TRANS_MIN_TM, 2.0f); 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 * Minimum altitude for fixed-wing flight. When the vehicle is in fixed-wing mode
* the vehicle will transition back to MC mode and enter failsafe RTL * 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 * @unit m
* @min 0.0 * @min 0.0
@@ -276,8 +277,8 @@ PARAM_DEFINE_INT32(VT_FW_QC_R, 0);
/** /**
* Quad-chute maximum height * Quad-chute maximum height
* *
* Maximum height above the ground (if available, otherwhise above * Maximum height above the ground (if available, otherwise above
* home if available, otherwise above the local origin) where triggering a quadchute is possible. * 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. * At high altitudes there is a big risk to deplete the battery and therefore crash if quad-chuting there.
* *
* @unit m * @unit m
@@ -288,7 +289,7 @@ PARAM_DEFINE_INT32(VT_FW_QC_R, 0);
PARAM_DEFINE_INT32(VT_FW_QC_HMAX, 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. * The duration of the front transition when there is no airspeed feedback available.
* *