From 86aacfb5da2c23132694be9a307e89d94574a868 Mon Sep 17 00:00:00 2001 From: PX4 Jenkins Date: Wed, 21 Mar 2018 04:41:16 +0000 Subject: [PATCH] Update PX4 Firmware metadata Wed Mar 21 04:41:16 UTC 2018 --- .../PX4/PX4ParameterFactMetaData.xml | 94 ++++++++++++++----- 1 file changed, 73 insertions(+), 21 deletions(-) diff --git a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml index 7d796c689..4fd9a8141 100644 --- a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml +++ b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml @@ -1925,6 +1925,78 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi modules/fw_att_control + + Pitch trim increment for flaps configuration + This increment is added to the pitch trim whenever flaps are fully deployed. + -0.25 + 0.25 + 2 + 0.01 + modules/fw_att_control + + + Pitch trim increment at maximum airspeed + This increment is added to TRIM_PITCH when airspeed is FW_AIRSP_MAX. + -0.25 + 0.25 + 2 + 0.01 + modules/fw_att_control + + + Pitch trim increment at minimum airspeed + This increment is added to TRIM_PITCH when airspeed is FW_AIRSPD_MIN. + -0.25 + 0.25 + 2 + 0.01 + modules/fw_att_control + + + Roll trim increment for flaps configuration + This increment is added to TRIM_ROLL whenever flaps are fully deployed. + -0.25 + 0.25 + 2 + 0.01 + modules/fw_att_control + + + Roll trim increment at maximum airspeed + This increment is added to TRIM_ROLL when airspeed is FW_AIRSP_MAX. + -0.25 + 0.25 + 2 + 0.01 + modules/fw_att_control + + + Roll trim increment at minimum airspeed + This increment is added to TRIM_ROLL when airspeed is FW_AIRSPD_MIN. + -0.25 + 0.25 + 2 + 0.01 + modules/fw_att_control + + + Yaw trim increment at maximum airspeed + This increment is added to TRIM_YAW when airspeed is FW_AIRSP_MAX. + -0.25 + 0.25 + 2 + 0.01 + modules/fw_att_control + + + Yaw trim increment at minimum airspeed + This increment is added to TRIM_YAW when airspeed is FW_AIRSPD_MIN. + -0.25 + 0.25 + 2 + 0.01 + modules/fw_att_control + Scale factor for flaperons 0.0 @@ -2406,7 +2478,7 @@ Set to 0 to disable heading hold Scale throttle by pressure change Automatically adjust throttle to account for decreased air density at higher altitudes. Start with a scale factor of 1.0 and adjust for different propulsion systems. When flying without airspeed sensor this will help to keep a constant performance over large altitude ranges. The default value of 0 will disable scaling. 0.0 - 2.0 + 10.0 1 0.1 modules/fw_pos_control_l1 @@ -4251,16 +4323,6 @@ default 1.5 turns per second 0.1 modules/mc_att_control - - Pitch time constant - Reduce if the system is too twitchy, increase if the response is too slow and sluggish. - 0.15 - 0.25 - s - 2 - 0.01 - modules/mc_att_control - Pitch rate integrator limit Pitch rate integrator limit. Can be set to increase the amount of integrator available to counteract disturbances or reduced to improve settling time after large pitch moment trim changes. @@ -4331,16 +4393,6 @@ default 1.5 turns per second 0.1 modules/mc_att_control - - Roll time constant - Reduce if the system is too twitchy, increase if the response is too slow and sluggish. - 0.15 - 0.25 - s - 2 - 0.01 - modules/mc_att_control - Roll rate integrator limit Roll rate integrator limit. Can be set to increase the amount of integrator available to counteract disturbances or reduced to improve settling time after large roll moment trim changes. -- 2.22.0