| Commit message (Collapse) | Author | Age |
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When the 3.3V and 5V values shift relative to each other (usually due
to changes in power consumption), the measured acceleration will
appear to shift. This patch converts the 3.3V referenced acceleration
value into a 5V referenced acceleration, eliminating this error.
Signed-off-by: Keith Packard <keithp@keithp.com>
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This stores the address of the desired sample in a local variable and
then fetches through that. Saves quite a few instructions.
Signed-off-by: Keith Packard <keithp@keithp.com>
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Instead of having everyone wait on the raw ADC ring, have the flight
code wait on that and have everyone else wait for the flight code to
finish looking at the data and move its pointer forwards.
Signed-off-by: Keith Packard <keithp@keithp.com>
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Slightly reduces code space.
Uncalibrated accelerometer now enters invalid state as well.
Signed-off-by: Mike Beattie <mike@ethernal.org>
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Chose invalid flight mode instead of idle to give user feedback.
Signed-off-by: Mike Beattie <mike@ethernal.org>
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When detecting flight or idle mode, this should indicate
that accel cal values are out of whack.
Signed-off-by: Mike Beattie <mike@ethernal.org>
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This lets us use a simple shift instead of a divide, saving a huge
amount of code space.
Signed-off-by: Keith Packard <keithp@keithp.com>
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These are all initialized in the ao_flight_drogue state transition.
Signed-off-by: Keith Packard <keithp@keithp.com>
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Presumably left-over debugging code.
Signed-off-by: Keith Packard <keithp@keithp.com>
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This wakes up the two GPS reporting tasks and gets them to report out
any existing GPS data to the log file. To make sure the timestamps in
that GPS data are accurate, this also records GPS time on receipt of
the GPS data instead of when that is logged.
Signed-off-by: Keith Packard <keithp@keithp.com>
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This allows you to override the flight mode detection code in case the
accelerometer calibration is broken somehow. Hold the SPI clock shoted
to ground until the LED comes on, then remove it.
Signed-off-by: Keith Packard <keithp@keithp.com>
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Detecting that the rocket has landed is required for the system to
flush the eeprom log and re-enable the RDF beacon. This patch changes
the landed state entry requirements for the accelerometer to require
only that the accelerometer stay within a quarter of a g (down from
1/10g) and changes the testing interval from 20 seconds to 5
seconds.
The requirement that the barometric altitude be within 1000m of the
launch altitude and that the barometer change by no more than 0.05kPa
are unchanged.
Signed-off-by: Keith Packard <keithp@keithp.com>
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Calibration now uses two values, one upside right and the other upside
down instead of a single horizontal value. This allows the use of
other accelerometers and compensates for variations in the divider
circuit to provide more accurate data.
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This splits the packet code into master/slave halves and hooks the
slave side up to the getchar/putchar/flush logic in ao_stdio.c
Signed-off-by: Keith Packard <keithp@keithp.com>
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__reentrant causes the compiler to place args and locals on the stack
instead of in the data segment.
Signed-off-by: Keith Packard <keithp@keithp.com>
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It's pretty much impossible to RDF the rocket during flight, and it
interferes with the telemetry data stream. Leave it enabled on the pad
so that radios can be tested, and then re-enable it once the rocket
has landed.
This patch also turns the rdf 'on' time into a parameter so it can be
changed, and then sets that parameter to 500ms, once every 5 seconds.
Signed-off-by: Keith Packard <keithp@keithp.com>
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Tracking the rocket on the ground may be easier using tones than using
the digital data stream, so we'll try that and see what we think.
This reverts commit 3a3bfd471a868d546d83cdc431b53c8f5208edb9.
Signed-off-by: Keith Packard <keithp@keithp.com>
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Signed-off-by: Keith Packard <keithp@keithp.com>
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