peabody124
11f2b1a8dc
Flight/Stabilization: Dont cap error at maximum stabilization value - that is to scale control throws. Create another variable if we want this.
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git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1676 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-09-17 18:15:02 +00:00
peabody124
41b7a99883
Flight/Stabilization: Yaw rate stabilization error should be normalized by dt
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git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1669 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-09-17 02:00:55 +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
andrew
65dc5e9b04
Yaw stabilisation for the simple algorithm was calculating the error and not taking into account that 350º error is the same as -10º error.
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The resultant error could range from -360º -> +360º
Since this is only used for Helicopters / multi rotors, and the aircraft can rotate in any direction, I added the modulo logic so that it is now from -180º -> +180º this should now take quickest path to correct the error.
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1464 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-08-30 01:20:43 +00:00
andrew
2361af19fb
First attempt at ccpm mixing for single rotor helicopter.
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This has throttle and pitch curves implemented and can be configured for many swashplate configurations.
This has flown a 450 clone (with training wheels) and the ccpm worked well.
Still need to neaten up some stuff and work out how to implement yaw stabilisation in manual mode.
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1412 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-08-26 06:00:57 +00:00
corvus
02a78f0470
moved Vassilis stabilization module as of r1153 into Stabilization/simple
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git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1173 ebee16cc-31ac-478f-84a7-5cbb03baadba
2010-07-28 15:03:55 +00:00
