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Diffstat (limited to 'src/core/ao_sample.c')
-rw-r--r-- | src/core/ao_sample.c | 214 |
1 files changed, 0 insertions, 214 deletions
diff --git a/src/core/ao_sample.c b/src/core/ao_sample.c deleted file mode 100644 index 2bf9632f..00000000 --- a/src/core/ao_sample.c +++ /dev/null @@ -1,214 +0,0 @@ -/* - * Copyright © 2011 Keith Packard <keithp@keithp.com> - * - * This program is free software; you can redistribute it and/or modify - * it under the terms of the GNU General Public License as published by - * the Free Software Foundation; version 2 of the License. - * - * This program is distributed in the hope that it will be useful, but - * WITHOUT ANY WARRANTY; without even the implied warranty of - * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU - * General Public License for more details. - * - * You should have received a copy of the GNU General Public License along - * with this program; if not, write to the Free Software Foundation, Inc., - * 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA. - */ - -#ifndef AO_FLIGHT_TEST -#include "ao.h" -#endif - -/* - * Current sensor values - */ - -__pdata uint16_t ao_sample_tick; /* time of last data */ -__pdata int16_t ao_sample_pres; -__pdata int16_t ao_sample_alt; -__pdata int16_t ao_sample_height; -#if HAS_ACCEL -__pdata int16_t ao_sample_accel; -#endif - -__data uint8_t ao_sample_adc; - -/* - * Sensor calibration values - */ - -__pdata int16_t ao_ground_pres; /* startup pressure */ -__pdata int16_t ao_ground_height; /* MSL of ao_ground_pres */ - -#if HAS_ACCEL -__pdata int16_t ao_ground_accel; /* startup acceleration */ -__pdata int16_t ao_accel_2g; /* factory accel calibration */ -__pdata int32_t ao_accel_scale; /* sensor to m/s² conversion */ -#endif - -static __pdata uint8_t ao_preflight; /* in preflight mode */ - -static __pdata uint16_t nsamples; -__pdata int32_t ao_sample_pres_sum; -#if HAS_ACCEL -__pdata int32_t ao_sample_accel_sum; -#endif - -static void -ao_sample_preflight(void) -{ - /* startup state: - * - * Collect 512 samples of acceleration and pressure - * data and average them to find the resting values - */ - if (nsamples < 512) { -#if HAS_ACCEL - ao_sample_accel_sum += ao_sample_accel; -#endif - ao_sample_pres_sum += ao_sample_pres; - ++nsamples; - } else { - ao_config_get(); -#if HAS_ACCEL - ao_ground_accel = ao_sample_accel_sum >> 9; - ao_accel_2g = ao_config.accel_minus_g - ao_config.accel_plus_g; - ao_accel_scale = to_fix32(GRAVITY * 2 * 16) / ao_accel_2g; -#endif - ao_ground_pres = ao_sample_pres_sum >> 9; - ao_ground_height = ao_pres_to_altitude(ao_ground_pres); - ao_preflight = FALSE; - } -} - -uint8_t -ao_sample(void) -{ - ao_wakeup(DATA_TO_XDATA(&ao_sample_adc)); - ao_sleep(DATA_TO_XDATA(&ao_adc_head)); - while (ao_sample_adc != ao_adc_head) { - __xdata struct ao_adc *ao_adc; - - /* Capture a sample */ - ao_adc = &ao_adc_ring[ao_sample_adc]; - ao_sample_tick = ao_adc->tick; - ao_sample_pres = ao_adc->pres; - ao_sample_alt = ao_pres_to_altitude(ao_sample_pres); - ao_sample_height = ao_sample_alt - ao_ground_height; -#if HAS_ACCEL - ao_sample_accel = ao_adc->accel; -#if HAS_ACCEL_REF - /* - * Ok, the math here is a bit tricky. - * - * ao_sample_accel: ADC output for acceleration - * ao_accel_ref: ADC output for the 5V reference. - * ao_cook_accel: Corrected acceleration value - * Vcc: 3.3V supply to the CC1111 - * Vac: 5V supply to the accelerometer - * accel: input voltage to accelerometer ADC pin - * ref: input voltage to 5V reference ADC pin - * - * - * Measured acceleration is ratiometric to Vcc: - * - * ao_sample_accel accel - * ------------ = ----- - * 32767 Vcc - * - * Measured 5v reference is also ratiometric to Vcc: - * - * ao_accel_ref ref - * ------------ = ----- - * 32767 Vcc - * - * - * ao_accel_ref = 32767 * (ref / Vcc) - * - * Acceleration is measured ratiometric to the 5V supply, - * so what we want is: - * - * ao_cook_accel accel - * ------------- = ----- - * 32767 ref - * - * - * accel Vcc - * = ----- * --- - * Vcc ref - * - * ao_sample_accel 32767 - * = ------------ * ------------ - * 32767 ao_accel_ref - * - * Multiply through by 32767: - * - * ao_sample_accel * 32767 - * ao_cook_accel = -------------------- - * ao_accel_ref - * - * Now, the tricky part. Getting this to compile efficiently - * and keeping all of the values in-range. - * - * First off, we need to use a shift of 16 instead of * 32767 as SDCC - * does the obvious optimizations for byte-granularity shifts: - * - * ao_cook_accel = (ao_sample_accel << 16) / ao_accel_ref - * - * Next, lets check our input ranges: - * - * 0 <= ao_sample_accel <= 0x7fff (singled ended ADC conversion) - * 0x7000 <= ao_accel_ref <= 0x7fff (the 5V ref value is close to 0x7fff) - * - * Plugging in our input ranges, we get an output range of 0 - 0x12490, - * which is 17 bits. That won't work. If we take the accel ref and shift - * by a bit, we'll change its range: - * - * 0xe000 <= ao_accel_ref<<1 <= 0xfffe - * - * ao_cook_accel = (ao_sample_accel << 16) / (ao_accel_ref << 1) - * - * Now the output range is 0 - 0x9248, which nicely fits in 16 bits. It - * is, however, one bit too large for our signed computations. So, we - * take the result and shift that by a bit: - * - * ao_cook_accel = ((ao_sample_accel << 16) / (ao_accel_ref << 1)) >> 1 - * - * This finally creates an output range of 0 - 0x4924. As the ADC only - * provides 11 bits of data, we haven't actually lost any precision, - * just dropped a bit of noise off the low end. - */ - ao_sample_accel = (uint16_t) ((((uint32_t) ao_sample_accel << 16) / (ao_accel_ref[ao_sample_adc] << 1))) >> 1; - if (ao_config.pad_orientation != AO_PAD_ORIENTATION_ANTENNA_UP) - ao_sample_accel = 0x7fff - ao_sample_accel; - ao_adc->accel = ao_sample_accel; -#else - if (ao_config.pad_orientation != AO_PAD_ORIENTATION_ANTENNA_UP) { - ao_sample_accel = 0x7fff - ao_sample_accel; - ao_adc->accel = ao_sample_accel; - } -#endif -#endif - - if (ao_preflight) - ao_sample_preflight(); - else - ao_kalman(); - ao_sample_adc = ao_adc_ring_next(ao_sample_adc); - } - return !ao_preflight; -} - -void -ao_sample_init(void) -{ - nsamples = 0; - ao_sample_pres_sum = 0; - ao_sample_pres = 0; -#if HAS_ACCEL - ao_sample_accel_sum = 0; - ao_sample_accel = 0; -#endif - ao_sample_adc = ao_adc_head; - ao_preflight = TRUE; -} |