4 Commits

Author	SHA1	Message	Date
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. ... 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. ... 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. ... 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 ... git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@1173 ebee16cc-31ac-478f-84a7-5cbb03baadba	2010-07-28 15:03:55 +00:00