Now that every bootloader build has a board info blob,
make all fw and bl images use it.
The following MACROS are removed:
BOARD_TYPE, BOARD_REVISION, BOOTLOADER_VERSION,
START_OF_USER_CODE, HW_TYPE
These values are now ONLY available from the bootloader
flash via the pios_board_info_blob symbol. These values
must not be #defined or otherwise hard-coded into the
firmware in any way. The bootloader flash is the only
valid source for this information.
NOTE: To ensure that we have an upgrade path from an
old bootloader (without board_info_blob) to a
new bootloader (with board_info_blob), it is
essential that the bu_* targets do not depend
on (or validate) the board_info_blob being present
in the bootloader flash.
Add (temporarily disabled) hooks for the rotational misalignment between the accelerometer and magnetometer.
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@3151 ebee16cc-31ac-478f-84a7-5cbb03baadba
data. I don't like this but because of the way the calibration routine works
(sets all gains to 1) this makes the values so far out or range the EKF doesn't
get to run and the mag wasn't previously being updated.
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2765 ebee16cc-31ac-478f-84a7-5cbb03baadba
(which is good) but that stops the comms polling. This makes it happen
ocassionally but not too much.
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2335 ebee16cc-31ac-478f-84a7-5cbb03baadba
range of NaN. This would reflect a race condition probably from the SPI
interaction.
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2334 ebee16cc-31ac-478f-84a7-5cbb03baadba
settings but only be used when home location is valid. Also discard any mag
data that is all zeros although we shouldn't see this.
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2283 ebee16cc-31ac-478f-84a7-5cbb03baadba
little aggressive. Also increased the drift rate of the gyro bias per Sambas'
testing (thanks) although not to the levels required for flying through 40 deg
C transitions.
Made the dump_ekf function handle both numbers of states
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2282 ebee16cc-31ac-478f-84a7-5cbb03baadba
bias as gravity vector facing down (bad for planes) which is diabled by
default.
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2232 ebee16cc-31ac-478f-84a7-5cbb03baadba
than the ekf runs and also be more tolerant of timing jitter
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2191 ebee16cc-31ac-478f-84a7-5cbb03baadba
from the AHRS code (which will facilitate code integration with new INS) and
also will help set up a fifo queue for the downsampled data to allow gyro data
output from AHRS faster than EKF output. Also decreased ADC interrupt priority
so the SPI comms don't drop out.
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2190 ebee16cc-31ac-478f-84a7-5cbb03baadba
bias correction. This is useful for stabilization to get rid of the gyro bias.
Making it an option is important for calibration.
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2189 ebee16cc-31ac-478f-84a7-5cbb03baadba
bounded. Velocity variance still comes from AHRSCalibration.
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2186 ebee16cc-31ac-478f-84a7-5cbb03baadba
velocity to help stabilize attitude. In principle the mag should be fine but
in practice I need this.
git-svn-id: svn://svn.openpilot.org/OpenPilot/trunk@2160 ebee16cc-31ac-478f-84a7-5cbb03baadba
