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Code Issues Releases Activity
3,666 Commits 5 Branches 8 Tags 266 MiB
2d995dc2f7
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35 Commits

Author SHA1 Message Date
James Cotton
2d995dc2f7 OP-539: Don't call the gyro setting callback during init because it clears the 
gyro bias estimation.
 2011-07-05 22:27:03 -05:00
James Cotton
4c0245281d Now we store the gyro bias avoid quashing the initialization correction. 2011-06-25 12:32:06 -05:00
James Cotton
e6ad21d881 Make gyro bias in deg/s * 100 to calibrate more precisely. 2011-06-24 10:51:07 -05:00
James Cotton
ab7ff56d96 Compute initial gyro bias while calibrating to speed up convergence 2011-06-24 10:38:26 -05:00
James Cotton
0a4bbcc12e Added a field for initial gyro bias to speed up initialization. 2011-06-24 10:38:26 -05:00
dankers
5f32803763 Changed accelKp = 1; in 3C filter when calibrating bias when arming. Increase default yaw by 0.005 2011-05-17 04:15:28 +10:00
dankers
71d582495e On arm bias calibration terms now matches boot calibration terms 2011-05-16 00:16:19 +10:00
dankers
84e09031a7 Faster attitude calc, be much more aggressive with working out bias. 
Change AccelkP to 0.05 to give accels more influence, just balacing out the 3C filter.

Change stab setting to be a better default fopr most Quads.
 2011-05-15 05:58:58 +10:00
James Cotton
dbf8a77a94 Now there are other attitude settings (like rotation angle) make sure these are 
loaded right away at power up
 2011-05-13 07:24:44 -05:00
James Cotton
4ec0263dfc OP-476: If AttitudeSettings.ZeroDuringArming is true, then while arming (1 
second) it will speed up the estimate of gyro bias.
 2011-05-07 15:29:21 -05:00
James Cotton
7e418866be Update the AttitudeSetting object to make the board rotation more human 
readable and update the GCS fields appropriately.
 2011-05-05 13:04:56 -05:00
peabody124
3afdc7e41c CC-24: Rotate the CC board at any angle relative to "flat and level" with GCS 
config plugin updates.  Has not been tested in flight yet although seems
sensible so please be careful when using this code.

git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@3166 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-04-15 06:37:16 +00:00
peabody124
a57c289b3a CC-24: Support mounting CC at any angle by applying a rotation. Now need to 
rotate sensors to make sure stabilization behaves well so don't use till then.

git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@3100 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-03-29 02:15:57 +00:00
peabody124
bd5925d526 CC-35: Separate term for CC yaw bias rate and others 
Note: AttitudeSettings changed so you'll need to re-zero it

git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@3090 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-03-28 18:42:48 +00:00
chebuzz
2e5863281c CC/Stabilization - Fix attitude bias not being applied over all sampled quantities 
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@3065 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-03-24 17:12:04 +00:00
osnwt
8d085552fb CC: Modules/Attitude/attitude.c: unused headers removed (do we have another?) 
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2967 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-03-04 21:12:37 +00:00
osnwt
e9d507dd3e CC: Fixed compilation error after uavobject rename 
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2966 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-03-04 20:56:58 +00:00
peabody124
ea390d0b90 CC-26: Add accel bias term. Note it's units are LSB, not m/s^s 
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2895 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-02-26 22:21:44 +00:00
pip
9a2bdac49c Reduced CC CPU usage from 57% to 46% by moving the floating point multiplies outside of the accelerometer downsample/averaging loop in the updateSensors() function. 
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2809 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-02-19 09:33:03 +00:00
peabody124
8498512855 CC-20 Attitude initialization: Make sure no divide by 0 condition possible 
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2761 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-02-08 16:34:55 +00:00
peabody124
9f71f4121c CC-18 Attitude: Change units to proper engineering ones. An accelKp=1 means 
that it will completely follow the accel attitude each cycle and is way too
high.  Ki=1 means the gyro bias wil be correct by accels each cycle (way too
high).

git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2755 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-02-08 16:34:35 +00:00
peabody124
cfe295377c CC-18: Normalize the gravity vector to unity gain 
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2754 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-02-08 16:34:31 +00:00
peabody124
74cc7dbfc9 CC-20 Attitude: Jack up Kp and Ki values for first 5 seconds to force faster 
convergence of gyro bias, then the normal values can be lower.

git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2753 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-02-08 16:34:28 +00:00
peabody124
03fb82ad0a CC Attitude: Change when AttitudeRaw is set to end of attitude estimation, 
because this is what is determines when the Stabilization code executes.
Because we aren't oversampling gyros relative to the PID in CC we should set
the attitude first (computational time to do so is negligible).

Also change update rate to 500 Hz.

git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2750 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-02-08 16:34:18 +00:00
peabody124
e5b26bc67d More memory tweaks to keep CC flowing 
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2709 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-02-03 02:42:49 +00:00
peabody124
fedadb1275 CC-8: Move the queue registration into the ADC PIOS driver to allow other 
functions to use it easily

Conflicts:

	flight/Modules/Attitude/attitude.c

git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2707 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-02-03 02:42:43 +00:00
peabody124
810fa70856 UAVObjects: Remove the raw versus filtered fields in the sensor data. Save 
some memory.

git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2706 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-02-03 02:42:39 +00:00
peabody124
c95a6447bf CC-8 Whenever the gyro data is updated the callback now pushes the data onto a 
queue, which update sensors waits for.  This confirms one update per gyro
update.  All available accel data will be pulled off each time.

git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2705 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-02-03 02:42:33 +00:00
peabody124
986e124202 CC-7 Reverse order of two lines so that yaw bias converges instead of diverges 
:-)

git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2693 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-02-02 09:16:28 +00:00
peabody124
265737427b CC-7: Make the gyro scale adjustable (for now at least, this was largely for 
debugging, let's compare values).

git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2692 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-02-02 08:57:42 +00:00
peabody124
1663a838ff CC-7 Full complimentary filter ala Mahoney paper using quaternion 
representation.  Also improved gyro bias initialization.

git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2691 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-02-02 08:57:38 +00:00
peabody124
b1e4b65f3d CC-1 Bigger oversampling window for CC sensor data 
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2667 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-02-01 02:18:31 +00:00
peabody124
1c6b51b704 UAVObjects/AttitudeSettinsg: Object for CC to tune the attitude estimation 
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2666 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-02-01 02:18:26 +00:00
peabody124
3f088bed8d CC-9 1. Improve the timings of the attitude estimation 
2. Disable FirmareIAP module in CC (somehow causes lockups when also using vTaskDelayUntil in Attitude WTF)
3. Make the SPI bus run a little faster so we can handle the 3200 Hz from accel
while running the filter at 333 Hz

git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2664 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-02-01 02:18:19 +00:00
peabody124
1cf7555b7d CC-10 Rename CCAttitude to Attitude. If there are alternative ones we will 
just have nested subdirectories of Attitude

git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2655 ebee16cc-31ac-478f-84a7-5cbb03baadba
 2011-02-01 02:17:40 +00:00