From d69cba5db95aae65d5cba7ee910b74f8db88737e Mon Sep 17 00:00:00 2001 From: bresch Date: Tue, 9 Oct 2018 10:10:15 +0200 Subject: [PATCH] FW trim - Fix typos in FW_DTRIM_R/P/Y_VMAX --- src/modules/fw_att_control/fw_att_control_params.c | 6 +++--- 1 file changed, 3 insertions(+), 3 deletions(-) diff --git a/src/modules/fw_att_control/fw_att_control_params.c b/src/modules/fw_att_control/fw_att_control_params.c index 61ee956b40..16d42fd305 100644 --- a/src/modules/fw_att_control/fw_att_control_params.c +++ b/src/modules/fw_att_control/fw_att_control_params.c @@ -675,7 +675,7 @@ PARAM_DEFINE_FLOAT(FW_DTRIM_Y_VMIN, 0.0f); /** * Roll trim increment at maximum airspeed * -* This increment is added to TRIM_ROLL when airspeed is FW_AIRSP_MAX. +* This increment is added to TRIM_ROLL when airspeed is FW_AIRSPD_MAX. * * @group FW Attitude Control * @min -0.25 @@ -688,7 +688,7 @@ PARAM_DEFINE_FLOAT(FW_DTRIM_R_VMAX, 0.0f); /** * Pitch trim increment at maximum airspeed * -* This increment is added to TRIM_PITCH when airspeed is FW_AIRSP_MAX. +* This increment is added to TRIM_PITCH when airspeed is FW_AIRSPD_MAX. * * @group FW Attitude Control * @min -0.25 @@ -701,7 +701,7 @@ PARAM_DEFINE_FLOAT(FW_DTRIM_P_VMAX, 0.0f); /** * Yaw trim increment at maximum airspeed * -* This increment is added to TRIM_YAW when airspeed is FW_AIRSP_MAX. +* This increment is added to TRIM_YAW when airspeed is FW_AIRSPD_MAX. * * @group FW Attitude Control * @min -0.25