From c065dbb0e908336c0e8a4e1e29bccf166a0dbd84 Mon Sep 17 00:00:00 2001 From: PX4BuildBot Date: Mon, 6 Jul 2020 14:31:32 +0000 Subject: [PATCH] Update PX4 Firmware metadata Mon Jul 6 14:31:32 UTC 2020 --- .../PX4/PX4ParameterFactMetaData.xml | 88 ++++++++++++++++++- 1 file changed, 84 insertions(+), 4 deletions(-) diff --git a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml index 79855cb9e..4b4c9ab7e 100644 --- a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml +++ b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml @@ -8302,7 +8302,7 @@ Particularly useful for testing different low-battery behaviour Rotation of magnetometer 0 relative to airframe An internal magnetometer will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero. -1 - 30 + 45 true Internal mag @@ -8332,6 +8332,26 @@ Particularly useful for testing different low-battery behaviour Roll 270°, Yaw 135° Pitch 90° Pitch 270° + Pitch 180°, Yaw 90° + Pitch 180°, Yaw 270° + Roll 90°, Pitch 90° + Roll 180°, Pitch 90° + Roll 270°, Pitch 90° + Roll 90°, Pitch 180° + Roll 270°, Pitch 180° + Roll 90°, Pitch 270° + Roll 180°, Pitch 270° + Roll 270°, Pitch 270° + Roll 90°, Pitch 180°, Yaw 90° + Roll 90°, Yaw 270° + Roll 90°, Pitch 68°, Yaw 293° + Pitch 315° + Roll 90°, Pitch 315° + Roll 270°, Yaw 180° + Roll 270°, Yaw 270° + Pitch 90°, Yaw 180° + Pitch 9°, Yaw 180° + Pitch 45° @@ -8383,7 +8403,7 @@ for current-based compensation [G/kA] Rotation of magnetometer 1 relative to airframe An internal magnetometer will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero. -1 - 30 + 45 true Internal mag @@ -8413,6 +8433,26 @@ for current-based compensation [G/kA] Roll 270°, Yaw 135° Pitch 90° Pitch 270° + Pitch 180°, Yaw 90° + Pitch 180°, Yaw 270° + Roll 90°, Pitch 90° + Roll 180°, Pitch 90° + Roll 270°, Pitch 90° + Roll 90°, Pitch 180° + Roll 270°, Pitch 180° + Roll 90°, Pitch 270° + Roll 180°, Pitch 270° + Roll 270°, Pitch 270° + Roll 90°, Pitch 180°, Yaw 90° + Roll 90°, Yaw 270° + Roll 90°, Pitch 68°, Yaw 293° + Pitch 315° + Roll 90°, Pitch 315° + Roll 270°, Yaw 180° + Roll 270°, Yaw 270° + Pitch 90°, Yaw 180° + Pitch 9°, Yaw 180° + Pitch 45° @@ -8464,7 +8504,7 @@ for current-based compensation [G/kA] Rotation of magnetometer 2 relative to airframe An internal magnetometer will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero. -1 - 30 + 45 true Internal mag @@ -8494,6 +8534,26 @@ for current-based compensation [G/kA] Roll 270°, Yaw 135° Pitch 90° Pitch 270° + Pitch 180°, Yaw 90° + Pitch 180°, Yaw 270° + Roll 90°, Pitch 90° + Roll 180°, Pitch 90° + Roll 270°, Pitch 90° + Roll 90°, Pitch 180° + Roll 270°, Pitch 180° + Roll 90°, Pitch 270° + Roll 180°, Pitch 270° + Roll 270°, Pitch 270° + Roll 90°, Pitch 180°, Yaw 90° + Roll 90°, Yaw 270° + Roll 90°, Pitch 68°, Yaw 293° + Pitch 315° + Roll 90°, Pitch 315° + Roll 270°, Yaw 180° + Roll 270°, Yaw 270° + Pitch 90°, Yaw 180° + Pitch 9°, Yaw 180° + Pitch 45° @@ -8545,7 +8605,7 @@ for current-based compensation [G/kA] Rotation of magnetometer 2 relative to airframe An internal magnetometer will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero. -1 - 30 + 45 true Internal mag @@ -8575,6 +8635,26 @@ for current-based compensation [G/kA] Roll 270°, Yaw 135° Pitch 90° Pitch 270° + Pitch 180°, Yaw 90° + Pitch 180°, Yaw 270° + Roll 90°, Pitch 90° + Roll 180°, Pitch 90° + Roll 270°, Pitch 90° + Roll 90°, Pitch 180° + Roll 270°, Pitch 180° + Roll 90°, Pitch 270° + Roll 180°, Pitch 270° + Roll 270°, Pitch 270° + Roll 90°, Pitch 180°, Yaw 90° + Roll 90°, Yaw 270° + Roll 90°, Pitch 68°, Yaw 293° + Pitch 315° + Roll 90°, Pitch 315° + Roll 270°, Yaw 180° + Roll 270°, Yaw 270° + Pitch 90°, Yaw 180° + Pitch 9°, Yaw 180° + Pitch 45° -- 2.22.0