Commit Graph
29 Commits
Author SHA1 Message Date
Hyon LimandHyon Lim 3bcd8c63f8 SMBus battery (a.k.a. smart battery) enhancement. (#14496)
* Enhancement: State of health, and max_error value is added. Both shows battery health of SMBUS smart battery.
 * Enhancement: BAT_C_MULT parameter is introduced. This is for high-current capable SMBUS-based battery.
As SMBUS only provides 16-bit for current, it could only be +-32768mA which is about +-32A.
But with proper treatment, it could be extended with little accuracy loss.
This factor can be set for individual battery system with available information.
    * Relative SOC introduced. Proper SMBUS battery should provide percentage of remaining battery
directly. Therefore it does not have to be computed like before.
    * State of Health introduced. Proper SMBUS battery should provide SOH value.
    * Max error: this shows estimation error of BMS.
 * Enhancement: With smart battery, precise estimation of time remaining is provided
with impedance track. It is unit of minute, so 60 seconds multiplied.
Update rate of this is not fast, but very useful.

Co-authored-by: Hyon Lim <lim@uvify.com>
2020-03-31 17:28:22 -04:00
Hyon Lim 0262a699c1 UVify Core board support and airframes (Draco, Draco-R, IFO) (#12337)
* also includes minor changes to make it easy to keep in sync with px4_fmu-v4
2019-08-23 17:02:25 -04:00
Hyon Lim b3f1adc54b SO3 estimator code has been cleaned 2013-11-29 02:35:49 +09:00
Hyon Lim bcd745fb0d SO(3) estimator and quaternion receive by mavlink implemented 2013-11-29 02:05:15 +09:00
Hyon Lim 9a4b57c352 Update fw_att_control_params.c 2013-11-20 03:04:53 +09:00
Hyon Lim ee985c70b3 Update fw_att_control_params.c
Minor comment error corrected.
2013-11-20 02:45:52 +09:00
Hyon Lim 1a3d17d4e7 Update sensor_params.c
Not necessarily modify this on initial.
2013-10-01 09:15:15 +09:00
Hyon Lim (Retina) 1c891d8a68 Airframe No. 21. 22 have been added.
That is for general ESC with PX4IO (frame geometry defined)
2013-09-25 02:17:06 +09:00
Hyon Lim (Retina) 4514045fb6 There were unintialized variables.
(control mode was not updated)

Also, new flags (xy_valid etc) were considered.
2013-09-25 02:12:55 +09:00
Hyon Lim (Retina) bfe22c1140 RC3 usually used as Throttle, but trim was set to 1500 by default.
It should be 1000 by default.
2013-09-25 02:02:51 +09:00
Hyon Lim a32b25eb52 Update 1001_rc_quad.hil
Default gain set
2013-09-19 05:33:57 +10:00
Hyon Lim (Retina) 36ffe2d694 Quadrotor HILS related RC script has been added 2013-09-19 04:29:46 +09:00
Hyon Lim (Retina) 6a6fe69371 Bug in so3 estimator related to R matrix 2013-08-31 03:23:03 +09:00
Hyon Lim (Retina) 9f2419698f Topic has been changed for quaternion-based attitude controller. 2013-08-31 03:22:19 +09:00
Hyon Lim (Retina) fff1856377 There was a bug in position_estimator_mc. Solved 2013-08-31 03:11:58 +09:00
Hyon Lim (Retina) 6537759dfc Add detailed documentation for SO3 gains tuning.
USB nsh has been removed.
2013-06-06 21:28:40 +10:00
Hyon Lim (Retina) 90fdf35ae5 GPL Licensed code has been removed 2013-05-29 00:59:20 +10:00
Hyon Lim (Retina) 7a2adb22eb Visualization code has been added. 2013-05-29 00:45:02 +10:00
Hyon Lim (Retina) 279028ede4 Merge branch 'master' of https://github.com/limhyon/Firmware 2013-05-29 00:35:02 +10:00
Hyon Lim (Retina) cc6c590af0 I finished to implement nonlinear complementary filter on the SO(3).
The previous problem was roll,pitch and yaw angle from quaternion.
Now it is fixed. 1-2-3 Euler representation is used.
Also accelerometer sign change has been applied.
2013-05-29 00:34:21 +10:00
Hyon Lim (Retina) f336a86baa I finished to implement nonlinear complementary filter on the SO(3).
The previous problem was roll,pitch and yaw angle from quaternion.
Now it is fixed. 1-2-3 Euler representation is used.
Also accelerometer sign change has been applied.
2013-05-29 00:29:31 +10:00
Hyon Lim (Retina) 13faf0d555 Merge remote-tracking branch 'upstream/master'
- Mikrokopter BLCTRL seems to be updated
 - HMC5883L calibration problem has been corrected.
    (This is because of RAM mis allocation?)
    See https://groups.google.com/forum/?fromgroups#!topic/px4users/yTYJiDBBKfo
 - Fixed wing control updated
    https://groups.google.com/forum/?fromgroups#!topic/px4users/s7owpvZN8UI
 - GPIO module has been removed.
 - STM32 DRV updated
2013-05-28 11:09:58 +10:00
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
Hyon Lim (Retina) 364d1a06e3 To use freeIMU processing visualization tool, I have implemented float number transmission over uart (default /dev/ttyS2, 115200)
But this not tested yet. I should.
2013-05-23 16:20:38 +10:00
Hyon Lim (Retina) f547044203 Roll pitch yaw should be verified again 2013-05-23 16:20:38 +10:00
Hyon Lim (Retina) 32bace0824 I do not know why roll angle is not correct. But system looks okay 2013-05-23 16:20:38 +10:00
Hyon Lim (Retina) 0c3412223b Fixed few minor bug 2013-05-23 16:20:38 +10:00
Hyon Lim (Retina) cd7b0f7aab I missed to add build command 2013-05-23 16:20:38 +10:00
Hyon Lim (Retina) 1caddb7bbb Initial work of so3 nonlinear complementary filter 2013-05-23 16:20:38 +10:00