From 8fe5ce4f65393cd7f15a5dbf1bb486a0e28af094 Mon Sep 17 00:00:00 2001 From: Silvan Fuhrer Date: Mon, 19 Jun 2023 10:22:33 +0200 Subject: [PATCH] VTOL: param description clean up Signed-off-by: Silvan Fuhrer --- .../vtol_att_control/vtol_att_control_params.c | 11 ++--------- 1 file changed, 2 insertions(+), 9 deletions(-) diff --git a/src/modules/vtol_att_control/vtol_att_control_params.c b/src/modules/vtol_att_control/vtol_att_control_params.c index 1361f1f5e6..34b1d598f3 100644 --- a/src/modules/vtol_att_control/vtol_att_control_params.c +++ b/src/modules/vtol_att_control/vtol_att_control_params.c @@ -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