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VTOL: param description clean up 

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
This commit is contained in:
Silvan Fuhrer 2023-06-19 10:22:33 +02:00
parent 327b7e611e
commit 8fe5ce4f65
1 changed files with 2 additions and 9 deletions
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11
src/modules/vtol_att_control/vtol_att_control_params.c
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@ -79,7 +79,6 @@ PARAM_DEFINE_FLOAT(VT_F_TRANS_DUR, 5.0f);
/**
* Maximum duration of a back transition
*
* Time in seconds used for a back transition maximally.
* Transition is also declared over if the groundspeed drops below MPC_XY_CRUISE.
*
* @unit s
@ -94,10 +93,6 @@ PARAM_DEFINE_FLOAT(VT_B_TRANS_DUR, 10.0f);
/**
* Target throttle value for the transition to fixed-wing flight.
*
* standard vtol: pusher
*
* tailsitter, tiltrotor: main throttle
*
* @min 0.0
* @max 1.0
* @increment 0.01
@ -109,7 +104,6 @@ PARAM_DEFINE_FLOAT(VT_F_TRANS_THR, 1.0f);
/**
* Approximate deceleration during back transition
*
* The approximate deceleration during a back transition in m/s/s
* Used to calculate back transition distance in an auto mode.
* For standard vtol and tiltrotors a controller is used to track this value during the transition.
*
@ -373,9 +367,8 @@ PARAM_DEFINE_FLOAT(VT_B_DEC_I, 0.1f);
/**
* Minimum pitch angle during hover.
*
* Minimum pitch angle during hover flight. If the desired pitch angle is is lower than this value
* then the fixed-wing forward actuation can be used to compensate for the missing thrust in forward direction
* (see VT_FW_TRHUST_EN)
* Any pitch setpoint below this value is translated to a forward force by the fixed-wing forward actuation if
* VT_FW_TRHUST_EN is set to 1.
*
* @unit deg
* @min -10.0