peabody124
4e6f100ae5
Flight: Swap to Les' code for main line
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git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1920 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-10-08 15:38:23 +00:00
peabody124
2dc40d11a1
Flight/Stabilization: Use the system clock to determine time from previous
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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
2010-10-01 12:33:29 +00:00
peabody124
3b015b41c5
Flight: Got a much nicer arming/disarming system going. Made it a separate flag in the end to allow testing the stabilization code with motors not running. Also changes maxRoll/maxPitch/maxYaw to uint8 to keep object size smaller - no reason for float precision for this.
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git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1660 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-09-16 15:41:11 +00:00
peabody124
a6e71177e4
AHRS: Yaw stabilization now supports rate stabilization or heading hold. Also need to cleanly support rate stabilization on all the other axis. Les suggested this be in manual mode which will require changing the logic somewhat (essentially for vtol it will always be running through the Stabilization module) in an aircraft dependent manner. An alternative would be a stabilization flag indicating to do full attitude hold, attitude + yaw stabilization, or all axis gyro stabilization. This would be my preference.
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git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1659 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-09-16 15:41:08 +00:00
peabody124
c376711405
Flight/Stabilization: Make the derivative account for the sampling time (dAngle/dt) for the PID loop since integral does and also make the integral bounds uavobject settings. It was originally bounded by constant/Ki but I'm not sure why as you change the gain of the error integral you also want to decrease the maximum error it can cause.
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git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1590 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-09-12 02:54:41 +00:00
cwabbott
d7a3ffb464
flight/PiOS.win32: update Makefile.win32 with new UAVObjects, also change UAVObject headers to have a newline at the end.
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git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1510 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-09-02 23:55:24 +00:00
peabody124
a0b21bef45
Flight: Got read only check working for UAVObjects and modified the ManualControl Module to use it. Edouard - please check over this.
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git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1427 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-08-27 00:15:48 +00:00
peabody124
a8df6e2c4d
OP-128 Flight Documentation: Added description to all the UAVObject (now mandatory) and changed the parser to populate this information into the autogenerated files. Also added a function to test if an object is read only for flight.
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Since there are a lot of autogenerated changes the important ones are:
flight/OpenPilot/UAVObjects/inc/uavobjecttemplate.h - added description and define to make the ObjectReadOnly query
flight/OpenPilot/UAVObjects/uavobjecttemplate.c
flight/OpenPilot/UAVObjects/uavobjectmanager.c - added the UAVObjReadOnly query
ground/src/libs/uavobjgenerator/uavobjectparser.cpp - added parsing of description field
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1425 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-08-27 00:15:42 +00:00
vassilis
c74eb2f0e9
OP-26 Flight/Stabilization First release of stabilization module. Tested using FlightGear, default tuning is for the HITL simulation. Works fairly well but a number of improvements can be made to aid tuning. The ManualControl settings must be first set as you would normally do for HITL simulation, flight mode is changed using the mode channel.
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git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@887 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-06-25 02:28:16 +00:00
vassilis
6b6740109e
OP-32 Flight Initial release of Actuator (ServoOut) and ManualControl (ServoIn) modules, still work in progress (not fully tested).
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git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@632 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-05-17 01:58:38 +00:00
