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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; -}  | 
