From b88e6b63022b926310d741f257844a0bad41933e Mon Sep 17 00:00:00 2001
From: Andrew Tridgell <tridge@samba.org>
Date: Tue, 25 Nov 2014 13:58:28 +1100
Subject: [PATCH] Plane: prepare for 3.2.0 release
---
ArduPlane/ArduPlane.pde | 2 +-
ArduPlane/release-notes.txt | 131 ++++++++++++++++++++++++++++++++++--
2 files changed, 127 insertions(+), 6 deletions(-)
diff --git a/ArduPlane/ArduPlane.pde b/ArduPlane/ArduPlane.pde
index 61fef59a7..262644797 100644
--- a/ArduPlane/ArduPlane.pde
+++ b/ArduPlane/ArduPlane.pde
@@ -1,6 +1,6 @@
/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
-#define THISFIRMWARE "ArduPlane V3.1.2beta3"
+#define THISFIRMWARE "ArduPlane V3.2.0"
/*
Lead developer: Andrew Tridgell
diff --git a/ArduPlane/release-notes.txt b/ArduPlane/release-notes.txt
index c519b8612..c21d63d51 100644
--- a/ArduPlane/release-notes.txt
+++ b/ArduPlane/release-notes.txt
@@ -1,10 +1,115 @@
-Release 3.1.2beta2, November 16th 2014
-----------------------------------
+Release 3.2.0, November 25th 2014
+---------------------------------
The ardupilot development team is proud to announce the release of
-version 3.1.2 of APM:Plane. This is a major release with a lot of
+version 3.2.0 of APM:Plane. This is a major release with a lot of
new features.
+The changes span a lot of different areas of the code, but arguably
+the most important changes are:
+
+ - automatic stall prevention code
+ - PX4IO based RC override code on FMU failure
+ - I2C crash bugfix
+ - new autoland code from Michael Day
+ - compass independent auto takeoff
+
+I'll go into each of these changes in a bit more detail.
+
+Automatic Stall Prevention
+--------------------------
+
+The automatic stall prevention code is code that uses the aerodynamic
+load factor (calculated from demanded bank angle) to adjust both the
+maximum roll angle and the minimum airspeed. You can enable/disable
+this code with the STALL_PREVENTION parameter which defaults to
+enabled.
+
+When in stabilised manual throttle modes this option has the effect of
+limiting how much bank angle you can demand when close to the
+configured minimum airspeed (from ARSPD_FBW_MIN). That means when in
+FBWA mode if you try to turn hard while close to ARSPD_FBW_MIN it will
+limit the bank angle to an amount that will keep the speed above
+ARSPD_FBW_MIN times the aerodynamic load factor. It will always allow
+you at bank at least 25 degrees however, to ensure you keep some
+maneuverability if the airspeed estimate is incorrect.
+
+When in auto-throttle modes (such as AUTO, RTL, CRUISE etc) it will
+additionally raise the minimum airspeed in proportion to the
+aerodynamic load factor. That means if a mission demands a sharp turn
+at low speed then initially the turn will be less sharp, and the TECS
+controller will add power to bring the airspeed up to a level that can
+handle the demanded turn. After the turn is complete the minimum
+airspeed will drop back to the normal level.
+
+This change won't completely eliminate stalls of course, but it should
+make them less likely if you properly configure ARSPD_FBW_MIN for your
+aircraft.
+
+PX4IO based RC override code
+----------------------------
+
+This releases adds support for PX4IO based RC override. This is a
+safety feature where the stm32 IO co-processor on the PX4 and Pixhawk
+will give the pilot manual control if the main ArduPilot
+micro-controller fails (or the autopilot code crashes). This is
+particularly useful when testing new code that may not be stable.
+
+As part of this new RC override support we also have a new
+OVERRIDE_CHAN parameter, which allows you to specify a RC input
+channel which can be used to test the RC override support. See the
+documentation on OVERRIDE_CHAN for details.
+
+I2C bugfix
+----------
+
+This release fixes another I2C bug in NuttX which could cause the
+Pixhawk to lock up under high I2C load with noise on I2C cables. This
+bug has caused at least two aircraft to crash, so it is an important
+fix. I hope this will be the last I2C crash bug we find in NuttX! An
+audit of the code was done to try to confirm that no more bugs of this
+type are present.
+
+New Autoland code
+-----------------
+
+This release incorporates some new autoland capabilities contributed
+by Michael Day. The key new feature is the ability to trigger an
+automatic landing when a RTL completes, which for the first time
+allows a user to setup their aircraft to land using only transmitter
+control.
+
+The way it works is there is a new parameter RTL_AUTOLAND. If that is
+set to 1 and the aircraft reaches its target location in an RTL it
+will look for DO_LAND_START mission item in the mission. If that is
+found then the aircraft will switch to AUTO starting at that section
+of the mission. The user sets up their land mission commands starting
+with a DO_LAND_START mission item.
+
+There is more to do in this autoland support. We have been discussing
+more advanced go-around capabilities and also better path planning for
+landing. The code in this release is an important first step though,
+and will be a good basis for future work.
+
+Compass independent takeoff code
+--------------------------------
+
+The auto-takeoff code has been changed to make it more independent of
+compass settings, allowing for reliable takeoff down a runway with
+poor compass offsets. The new takeoff code uses the gyroscope as the
+primary heading control for the first part of the takeoff, until the
+aircraft gains enough speed for a GPS heading to be reliable.
+
+Many thanks to all the contributors, especially:
+
+ - Paul and Jon for EKF and TECS updates
+ - Bret and Grant for stall prevention testing
+ - Michael for all his autoland work
+ - all the work on NavIO, PXF and Zynq by John, Victor, George and Siddarth
+ - The PX4 team for all the PX4 updates
+
+More complete list of changes:
+
- allow GCS to enable/disable PX4 safety switch
- make auto-takeoff independent of compass errors
- report gyro unhealthy if calibration failed
@@ -22,7 +127,7 @@ new features.
- added STALL_PREVENTION parameter
- fixed handling of TKOFF_THR_MAX parameter
- added ARSPD_SKIP_CAL parameter
- - fixed flaperon trim handling (WARNING: need to retrim flaperons)
+ - fixed flaperon trim handling (WARNING: may need to retrim flaperons)
- EKF robustness improvements, especially for MAG handling
- lots of HAL_Linux updates
- support wider range of I2C Lidars
@@ -32,6 +137,22 @@ new features.
- AP_Mount: added lead filter to improve servo gimbals
- Zynq and NavIO updates
- fixed preflight calibration to prevent losing 3D accel cal
+ - perform a gyro calibration when doing 3D accel cal
+ - added DO_CONTINUE_AND_CHANGE_ALT mission command
+ - added support for DO_FENCE_ENABLE mission command
+ - allow gyro calibration to take up to 30 seconds
+ - improved health checks in the EKF for DCM fallback
+
+Note: If you use flaperons you may need to re-trim them before you
+fly due to the change in flaperon trim handling.
+
+I hope that everyone enjoys flying this new APM:Plane release as much
+as we enjoyed producing it! It is a major milestone in the development
+of the fixed wing code for APM, and I think puts us in a great
+position for future development.
+
+Happy flying!
+
Release 3.1.1, September 12th 2014
@@ -665,5 +786,5 @@ as we enjoyed producing it! It is a major milestone in the development
of the fixed wing code for APM, and I think puts us in a great
position for future development.
-Happy flying!
+Happy flying!
--
GitLab