Hyon Lim (Retina) 4bf0505421 Test flight has been performed with nonlinear SO(3) attitude estimator. ...

Here are few observations:
 - When the system initialized, roll angle is initially reversed.
   As filter converged, it becomes normal.
 - I put a negative sign on roll, yaw. It should naturally has right
   sign, but I do not know why for now. Let me investigate again.
 - Gain : I do not know what gain is good for quadrotor flight.
   Let me take a look Ardupilot gain in the later.

Anyway, you can fly with this attitude estimator.

2013-05-23 16:20:38 +10:00

..

drivers

Hotfix: Changed alarms back to what they originally were designed for: Traps to later see if condition was once violated. Currente status can be read through the status flags

2013-05-21 09:14:22 +02:00

examples

More example fixes

2013-05-13 08:28:36 +02:00

include

VA args now supported by MAVLink text messages

2013-05-21 09:14:22 +02:00

modules

Test flight has been performed with nonlinear SO(3) attitude estimator.

2013-05-23 16:20:38 +10:00

systemcmds

VA args now supported by MAVLink text messages

2013-05-21 09:14:22 +02:00