As this changes UAVObjects both flight and GCS software will need to be recompiled to stay in sync.
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2303 ebee16cc-31ac-478f-84a7-5cbb03baadba
As this changes UAVObjects both flight and GCS software will need to be recompiled to stay in sync.
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2302 ebee16cc-31ac-478f-84a7-5cbb03baadba
Added:
Battery
Flight Time
I2C
GPS
Also added new alarm state of "Uninitialised"
no code to set these alarms yet.
As this changes UAVObjects both flight and GCS software will need to be recompiled to stay in sync.
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2294 ebee16cc-31ac-478f-84a7-5cbb03baadba
sometimes thrown, and made errors not lock it up by default. It works for me,
but since this has historically been associated with lots of lock ups please
check your systems carefully.
PiOS/I2C: Make the bus by default try to recover from errors instead of locking
up
PiOS/I2C: After a bus error and clocking all previous data create a STOP
condition to make sure bus is released (note, this also requires creating a
START condition first)
PiOS/I2C: If the same event hits the I2C bus twice in a row then disregard
second one, there is no situation where we should get the same event multiple
times that matters and this gets us out really quickly to catch the real
events. I was seeing this with repeated 0x70084 which means byte transmitted.
This is related to STM32 bugs in the IRQ timings I believe.
PiOS/I2C: 1) Mask out some bits we don't care about in the event flags
2) Don't lock up if the give semaphore fails, although why it does is strange
3) Recover from bus failure through the "auto" state path instead of just
coding state
PiOS/I2C: Change the reset bus code to follow
http://www.analog.com/static/imported-files/application_notes/54305147357414AN686_0.pdf
(thanks for the reference Neontangerine). Although this may actually NOT clear
the bus the first time through, subsequent bus errors should eventually clock
it out. The up side is it is less likely to clock a bunch of 1s into an ESC
and make it run up.
PiOS/I2C: Some cleaned up code for getting a snippet of the history when
something strange happens
PiOS/I2C: Export logging information from I2C through a UAV object
PiOS/I2C: Improve the diagnostic information
PiOS/I2C: Need to handle the event 0x30084. This seems to happen between a
byte transmitted and new byte started
PiOS/I2C: Handle the NACK condition by simply going to the stopping state.
PiOS/I2C: Add a new NACK state to handle sending the STOP signal after a NACK
following the STM documentation. Other error conditions still are not dealt
with.
PiOS/I2C: Should handle the NACK condition from all the write cases. Need to
think about read cases
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2239 ebee16cc-31ac-478f-84a7-5cbb03baadba
BEWARE: I have not flown my quad with this code, so please be careful, test, and report!
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2234 ebee16cc-31ac-478f-84a7-5cbb03baadba
bias correction. This is useful for stabilization to get rid of the gyro bias.
Making it an option is important for calibration.
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2189 ebee16cc-31ac-478f-84a7-5cbb03baadba
ManualControlSettings so that planes can disable the timeout
feature for gliding (holding roll on a plane not so good).
Note: This will require you to reconfigure your ManualControlSettings
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2185 ebee16cc-31ac-478f-84a7-5cbb03baadba
indoor from the name since it's used for both indoor and outdoor mode now.
Increased default value to 0.4 to better reflect the GPS accuracy.
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2156 ebee16cc-31ac-478f-84a7-5cbb03baadba
parallel for this update. Also removed comment for rawhid
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2012 ebee16cc-31ac-478f-84a7-5cbb03baadba
uavobjectgenerator to support multiple fields (thanks Les!). Also
changed default scale on mag to +/-6g
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1899 ebee16cc-31ac-478f-84a7-5cbb03baadba
so it can also change parameters of Stabilization. Please check your aircraft
behavior with this patch, but default behavior should be unchanged.
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1878 ebee16cc-31ac-478f-84a7-5cbb03baadba
fly (EKF rate up to a limit). Also, now the algorithm selects if you are
indoor or outdoor as well as if you use a mag indoor (if you do set the z
variance higher than it calibrates to).
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1841 ebee16cc-31ac-478f-84a7-5cbb03baadba
and removed the unused field from actuator settings (old setting time and all
the aircraft specific stuff).
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1820 ebee16cc-31ac-478f-84a7-5cbb03baadba
update since now drive by events. This means StabilizationSettings object
changing so write down your settings.
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1819 ebee16cc-31ac-478f-84a7-5cbb03baadba
Flight: Create PositionDesired (the active waypoint) UAVObject and make the FlightSituationActual no update since it not used.
Flight: New velocity desired object that passes information between the look computing the desired velocity and the PID loop to get it (updated at different rates)
UAVObjects/PositionActual: Remove unused GPS fields
UAVObjects/PositionActual VelocityActual: Split the velocity into a separate object. ALso make sure all the information telemetered around is in cm to avoid using floats.
UAVObject/GuidanceSettings: New guidance settings object for the guidance module
Flight/Posix: Add the new objects to the Posix sim
Flight/Guidance: Computes a desired velocity based on position error than runs a PID loop to control roll and pitch to achieve that velocity. All distances are in cm, and updated the PositionActual fields to reflect this and use int32.
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1760 ebee16cc-31ac-478f-84a7-5cbb03baadba
