diff options
Diffstat (limited to 'src/kernel')
| -rw-r--r-- | src/kernel/ao_flash_readout.c | 50 | ||||
| -rw-r--r-- | src/kernel/ao_flash_readout.h | 20 | ||||
| -rw-r--r-- | src/kernel/ao_flight.c | 11 | ||||
| -rw-r--r-- | src/kernel/ao_flight.h | 1 | ||||
| -rw-r--r-- | src/kernel/ao_kalman.c | 10 | ||||
| -rw-r--r-- | src/kernel/ao_product.c | 14 | ||||
| -rw-r--r-- | src/kernel/ao_pyro.c | 36 | ||||
| -rw-r--r-- | src/kernel/ao_sample.c | 83 | ||||
| -rw-r--r-- | src/kernel/ao_sample.h | 3 | ||||
| -rw-r--r-- | src/kernel/ao_usb.h | 21 | 
10 files changed, 203 insertions, 46 deletions
diff --git a/src/kernel/ao_flash_readout.c b/src/kernel/ao_flash_readout.c new file mode 100644 index 00000000..46b5ba7a --- /dev/null +++ b/src/kernel/ao_flash_readout.c @@ -0,0 +1,50 @@ +/* + * Copyright © 2018 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, either version 2 of the License, or + * (at your option) any later version. + * + * 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. + */ + +#include <ao.h> +#include <ao_usb.h> +#include <ao_flash_readout.h> + +#ifndef AO_FLASH_READOUT_BASE +#define AO_FLASH_READOUT_BASE	AO_BOOT_LOADER_BASE +#define AO_FLASH_READOUT_BOUND	AO_BOOT_APPLICATION_BOUND +#endif + +static void +ao_flash_readout(void) +{ +	uint8_t	*base = (uint8_t *) AO_FLASH_READOUT_BASE; +	uint8_t	*bound = (uint8_t *) AO_FLASH_READOUT_BOUND; +	uint8_t	*p = base; + +	for (;;) { +		ao_arch_block_interrupts(); +		while (!ao_usb_running) { +			p = base; +			ao_sleep(&ao_usb_running); +		} +		ao_arch_release_interrupts(); +		ao_flash_readout_putchar(*p++); +		if (p == bound) +			p = base; +	} +} + +static struct ao_task	ao_flash_readout_task; + +void +ao_flash_readout_init(void) +{ +	ao_add_task(&ao_flash_readout_task, ao_flash_readout, "flash_readout"); +} diff --git a/src/kernel/ao_flash_readout.h b/src/kernel/ao_flash_readout.h new file mode 100644 index 00000000..5eee53cc --- /dev/null +++ b/src/kernel/ao_flash_readout.h @@ -0,0 +1,20 @@ +/* + * Copyright © 2018 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, either version 2 of the License, or + * (at your option) any later version. + * + * 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. + */ + +#ifndef _AO_FLASH_READOUT_H_ +#define _AO_FLASH_READOUT_H_ + +void	ao_flash_readout_init(void); + +#endif /* _AO_FLASH_READOUT_H_ */ diff --git a/src/kernel/ao_flight.c b/src/kernel/ao_flight.c index cb02c454..c2700d20 100644 --- a/src/kernel/ao_flight.c +++ b/src/kernel/ao_flight.c @@ -48,7 +48,8 @@  /* Main flight thread. */  __pdata enum ao_flight_state	ao_flight_state;	/* current flight state */ -__pdata uint16_t		ao_boost_tick;		/* time of launch detect */ +__pdata uint16_t		ao_boost_tick;		/* time of most recent boost detect */ +__pdata uint16_t		ao_launch_tick;		/* time of first boost detect */  __pdata uint16_t		ao_motor_number;	/* number of motors burned so far */  #if HAS_SENSOR_ERRORS @@ -199,7 +200,7 @@ ao_flight(void)  				)  			{  				ao_flight_state = ao_flight_boost; -				ao_boost_tick = ao_sample_tick; +				ao_launch_tick = ao_boost_tick = ao_sample_tick;  				/* start logging data */  				ao_log_start(); @@ -233,7 +234,7 @@ ao_flight(void)  			 * deceleration, or by waiting until the maximum burn duration  			 * (15 seconds) has past.  			 */ -			if ((ao_accel < AO_MSS_TO_ACCEL(-2.5) && ao_height > AO_M_TO_HEIGHT(100)) || +			if ((ao_accel < AO_MSS_TO_ACCEL(-2.5)) ||  			    (int16_t) (ao_sample_tick - ao_boost_tick) > BOOST_TICKS_MAX)  			{  #if HAS_ACCEL @@ -269,7 +270,7 @@ ao_flight(void)  			 * number of seconds.  			 */  			if (ao_config.apogee_lockout) { -				if ((int16_t) (ao_sample_tick - ao_boost_tick) < +				if ((int16_t) (ao_sample_tick - ao_launch_tick) <  				    AO_SEC_TO_TICKS(ao_config.apogee_lockout))  					break;  			} @@ -310,7 +311,7 @@ ao_flight(void)  #if HAS_ACCEL  			else {  			check_re_boost: -				ao_coast_avg_accel = ao_coast_avg_accel - (ao_coast_avg_accel >> 6) + (ao_accel >> 6); +				ao_coast_avg_accel = ao_coast_avg_accel + ((ao_accel - ao_coast_avg_accel) >> 5);  				if (ao_coast_avg_accel > AO_MSS_TO_ACCEL(20)) {  					ao_boost_tick = ao_sample_tick;  					ao_flight_state = ao_flight_boost; diff --git a/src/kernel/ao_flight.h b/src/kernel/ao_flight.h index 6894fe59..005c7e84 100644 --- a/src/kernel/ao_flight.h +++ b/src/kernel/ao_flight.h @@ -40,6 +40,7 @@ enum ao_flight_state {  extern __pdata enum ao_flight_state	ao_flight_state;  extern __pdata uint16_t			ao_boost_tick; +extern __pdata uint16_t			ao_launch_tick;  extern __pdata uint16_t			ao_motor_number;  #if HAS_IMU || HAS_MMA655X diff --git a/src/kernel/ao_kalman.c b/src/kernel/ao_kalman.c index ac41085d..e4cc6d4b 100644 --- a/src/kernel/ao_kalman.c +++ b/src/kernel/ao_kalman.c @@ -45,7 +45,11 @@ static __pdata ao_k_t		ao_avg_height_scaled;  __xdata ao_v_t			ao_avg_height;  __pdata ao_v_t			ao_error_h; -#if !HAS_ACCEL +#if !HAS_ACCEL || AO_FLIGHT_TEST +#define AO_ERROR_H_SQ_AVG	1 +#endif + +#if AO_ERROR_H_SQ_AVG  __pdata ao_v_t			ao_error_h_sq_avg;  #endif @@ -85,7 +89,7 @@ ao_kalman_predict(void)  static void  ao_kalman_err_height(void)  { -#if !HAS_ACCEL +#if AO_ERROR_H_SQ_AVG  	ao_v_t	e;  #endif  	ao_v_t height_distrust; @@ -95,7 +99,7 @@ ao_kalman_err_height(void)  	ao_error_h = ao_sample_height - (ao_v_t) (ao_k_height >> 16); -#if !HAS_ACCEL +#if AO_ERROR_H_SQ_AVG  	e = ao_error_h;  	if (e < 0)  		e = -e; diff --git a/src/kernel/ao_product.c b/src/kernel/ao_product.c index c4df9f26..4c2d83ef 100644 --- a/src/kernel/ao_product.c +++ b/src/kernel/ao_product.c @@ -55,7 +55,7 @@ const char ao_product[] = AO_iProduct_STRING;  #define HEADER_LEN	       	9  #define CONTROL_CLASS_LEN	35 -#define DATA_LEN		(9 + 7 * AO_USB_HAS_OUT + 7 * AO_USB_HAS_IN + 7 * AO_USB_HAS_IN2) +#define DATA_LEN		(9 + 7 * AO_USB_HAS_OUT + 7 * AO_USB_HAS_IN + 7 * AO_USB_HAS_IN2 + 7 * AO_USB_HAS_IN3)  #define TOTAL_LENGTH		(HEADER_LEN + AO_USB_HAS_INT * CONTROL_CLASS_LEN + DATA_LEN)  #define NUM_INTERFACES		(AO_USB_HAS_INT + 1) @@ -141,7 +141,7 @@ AO_ROMCONFIG_SYMBOL(0x00aa) uint8_t ao_usb_descriptors [] =  	AO_USB_DESC_INTERFACE,  	AO_USB_HAS_INT,			/* bInterfaceNumber */  	0x00,				/* bAlternateSetting */ -	AO_USB_HAS_OUT + AO_USB_HAS_IN + AO_USB_HAS_IN2,	/* bNumEndPoints */ +	AO_USB_HAS_OUT + AO_USB_HAS_IN + AO_USB_HAS_IN2 + AO_USB_HAS_IN3,	/* bNumEndPoints */  	AO_USB_INTERFACE_CLASS_DATA,	/* bInterfaceClass = data */  	0x00,				/* bInterfaceSubClass */  	0x00,				/* bInterfaceProtocol */ @@ -177,6 +177,16 @@ AO_ROMCONFIG_SYMBOL(0x00aa) uint8_t ao_usb_descriptors [] =  	0x00,			/* bInterval */  #endif +#if AO_USB_HAS_IN3 +	/* Data EP in 3 */ +	0x07, +	AO_USB_DESC_ENDPOINT, +	AO_USB_IN3_EP|0x80,	/* bEndpointAddress */ +	0x02,			/* bmAttributes = bulk */ +	LE_WORD(AO_USB_IN_SIZE),/* wMaxPacketSize */ +	0x00,			/* bInterval */ +#endif +  	/* String descriptors */  	0x04,  	AO_USB_DESC_STRING, diff --git a/src/kernel/ao_pyro.c b/src/kernel/ao_pyro.c index e5c30eec..527112ac 100644 --- a/src/kernel/ao_pyro.c +++ b/src/kernel/ao_pyro.c @@ -81,6 +81,19 @@ int pyro_dbg;  #define DBG(...)  #endif +static angle_t +ao_sample_max_orient(void) +{ +	uint8_t	i; +	angle_t	max = ao_sample_orients[0]; + +	for (i = 1; i < AO_NUM_ORIENT; i++) { +		angle_t a = ao_sample_orients[i]; +		if (a > max) +			max = a; +	} +	return max; +}  /*   * Given a pyro structure, figure out   * if the current flight state satisfies all @@ -90,6 +103,9 @@ static uint8_t  ao_pyro_ready(struct ao_pyro *pyro)  {  	enum ao_pyro_flag flag, flags; +#if HAS_GYRO +	angle_t max_orient; +#endif  	flags = pyro->flags;  	while (flags != ao_pyro_none) { @@ -130,26 +146,28 @@ ao_pyro_ready(struct ao_pyro *pyro)  #if HAS_GYRO  		case ao_pyro_orient_less: -			if (ao_sample_orient <= pyro->orient_less) +			max_orient = ao_sample_max_orient(); +			if (max_orient <= pyro->orient_less)  				continue; -			DBG("orient %d > %d\n", ao_sample_orient, pyro->orient_less); +			DBG("orient %d > %d\n", max_orient, pyro->orient_less);  			break;  		case ao_pyro_orient_greater: -			if (ao_sample_orient >= pyro->orient_greater) +			max_orient = ao_sample_max_orient(); +			if (max_orient >= pyro->orient_greater)  				continue; -			DBG("orient %d < %d\n", ao_sample_orient, pyro->orient_greater); +			DBG("orient %d < %d\n", max_orient, pyro->orient_greater);  			break;  #endif  		case ao_pyro_time_less: -			if ((int16_t) (ao_time() - ao_boost_tick) <= pyro->time_less) +			if ((int16_t) (ao_time() - ao_launch_tick) <= pyro->time_less)  				continue; -			DBG("time %d > %d\n", (int16_t)(ao_time() - ao_boost_tick), pyro->time_less); +			DBG("time %d > %d\n", (int16_t)(ao_time() - ao_launch_tick), pyro->time_less);  			break;  		case ao_pyro_time_greater: -			if ((int16_t) (ao_time() - ao_boost_tick) >= pyro->time_greater) +			if ((int16_t) (ao_time() - ao_launch_tick) >= pyro->time_greater)  				continue; -			DBG("time %d < %d\n", (int16_t)(ao_time() - ao_boost_tick), pyro->time_greater); +			DBG("time %d < %d\n", (int16_t)(ao_time() - ao_launch_tick), pyro->time_greater);  			break;  		case ao_pyro_ascending: @@ -164,7 +182,7 @@ ao_pyro_ready(struct ao_pyro *pyro)  			break;  		case ao_pyro_after_motor: -			if (ao_motor_number == pyro->motor) +			if (ao_motor_number >= pyro->motor)  				continue;  			DBG("motor %d != %d\n", ao_motor_number, pyro->motor);  			break; diff --git a/src/kernel/ao_sample.c b/src/kernel/ao_sample.c index 61519478..f8012e34 100644 --- a/src/kernel/ao_sample.c +++ b/src/kernel/ao_sample.c @@ -50,6 +50,8 @@ __pdata gyro_t		ao_sample_roll;  __pdata gyro_t		ao_sample_pitch;  __pdata gyro_t		ao_sample_yaw;  __pdata angle_t		ao_sample_orient; +__pdata angle_t		ao_sample_orients[AO_NUM_ORIENT]; +__pdata uint8_t		ao_sample_orient_pos;  #endif  __data uint8_t		ao_sample_data; @@ -115,6 +117,53 @@ ao_sample_preflight_add(void)  	++nsamples;  } +#if HAS_GYRO +static void +ao_sample_set_all_orients(void) +{ +	int i; +	for (i = 0; i < AO_NUM_ORIENT; i++) +		ao_sample_orients[i] = ao_sample_orient; +	ao_sample_orient_pos = 0; +} + +static void +ao_sample_set_one_orient(void) +{ +	ao_sample_orients[ao_sample_orient_pos] = ao_sample_orient; +	ao_sample_orient_pos = (ao_sample_orient_pos + 1) % AO_NUM_ORIENT; +} + +static void +ao_sample_compute_orient(void) +{ +	/* Compute pitch angle from vertical by taking the pad +	 * orientation vector and rotating it by the current total +	 * rotation value. That will be a unit vector pointing along +	 * the airframe axis. The Z value will be the cosine of the +	 * change in the angle from vertical since boost. +	 * +	 * rot = ao_rotation * vertical * ao_rotation° +	 * rot = ao_rotation * (0,0,0,1) * ao_rotation° +	 *     = ((a.z, a.y, -a.x, a.r) * (a.r, -a.x, -a.y, -a.z)) .z +	 * +	 *     = (-a.z * -a.z) + (a.y * -a.y) - (-a.x * -a.x) + (a.r * a.r) +	 *     = a.z² - a.y² - a.x² + a.r² +	 * +	 * rot = ao_rotation * (0, 0, 0, -1) * ao_rotation° +	 *     = ((-a.z, -a.y, a.x, -a.r) * (a.r, -a.x, -a.y, -a.z)) .z +	 * +	 *     = (a.z * -a.z) + (-a.y * -a.y) - (a.x * -a.x) + (-a.r * a.r) +	 *     = -a.z² + a.y² + a.x² - a.r² +	 */ + +	float rotz; +	rotz = ao_rotation.z * ao_rotation.z - ao_rotation.y * ao_rotation.y - ao_rotation.x * ao_rotation.x + ao_rotation.r * ao_rotation.r; + +	ao_sample_orient = acosf(rotz) * (float) (180.0/M_PI); +} +#endif /* HAS_GYRO */ +  static void  ao_sample_preflight_set(void)  { @@ -138,7 +187,7 @@ ao_sample_preflight_set(void)  	ao_sample_pitch_sum = 0;  	ao_sample_yaw_sum = 0;  	ao_sample_roll_sum = 0; -	ao_sample_orient = 0; +	ao_sample_set_all_orients();  	struct ao_quaternion	orient; @@ -168,6 +217,9 @@ ao_sample_preflight_set(void)  	if (ao_orient_test)  		printf("\n\treset\n");  #endif	 + +	ao_sample_compute_orient(); +	ao_sample_set_all_orients();  #endif  	nsamples = 0;  } @@ -195,31 +247,6 @@ ao_sample_rotate(void)  	/* And normalize to make sure it remains a unit vector */  	ao_quaternion_normalize(&ao_rotation, &ao_rotation); -	/* Compute pitch angle from vertical by taking the pad -	 * orientation vector and rotating it by the current total -	 * rotation value. That will be a unit vector pointing along -	 * the airframe axis. The Z value will be the cosine of the -	 * change in the angle from vertical since boost. -	 * -	 * rot = ao_rotation * vertical * ao_rotation° -	 * rot = ao_rotation * (0,0,0,1) * ao_rotation° -	 *     = ((a.z, a.y, -a.x, a.r) * (a.r, -a.x, -a.y, -a.z)) .z -	 * -	 *     = (-a.z * -a.z) + (a.y * -a.y) - (-a.x * -a.x) + (a.r * a.r) -	 *     = a.z² - a.y² - a.x² + a.r² -	 * -	 * rot = ao_rotation * (0, 0, 0, -1) * ao_rotation° -	 *     = ((-a.z, -a.y, a.x, -a.r) * (a.r, -a.x, -a.y, -a.z)) .z -	 * -	 *     = (a.z * -a.z) + (-a.y * -a.y) - (a.x * -a.x) + (-a.r * a.r) -	 *     = -a.z² + a.y² + a.x² - a.r² -	 */ - -	float rotz; -	rotz = ao_rotation.z * ao_rotation.z - ao_rotation.y * ao_rotation.y - ao_rotation.x * ao_rotation.x + ao_rotation.r * ao_rotation.r; - -	ao_sample_orient = acosf(rotz) * (float) (180.0/M_PI); -  #if HAS_FLIGHT_DEBUG  	if (ao_orient_test) {  		printf ("rot %d %d %d orient %d     \r", @@ -229,7 +256,8 @@ ao_sample_rotate(void)  			ao_sample_orient);  	}  #endif - +	ao_sample_compute_orient(); +	ao_sample_set_one_orient();  }  #endif @@ -367,6 +395,7 @@ ao_sample_init(void)  	ao_sample_yaw = 0;  	ao_sample_roll = 0;  	ao_sample_orient = 0; +	ao_sample_set_all_orients();  #endif  	ao_sample_data = ao_data_head;  	ao_preflight = TRUE; diff --git a/src/kernel/ao_sample.h b/src/kernel/ao_sample.h index fbef031d..5ae389be 100644 --- a/src/kernel/ao_sample.h +++ b/src/kernel/ao_sample.h @@ -146,7 +146,10 @@ extern __pdata accel_t	ao_sample_accel_through;  extern __pdata gyro_t	ao_sample_roll;  extern __pdata gyro_t	ao_sample_pitch;  extern __pdata gyro_t	ao_sample_yaw; +#define AO_NUM_ORIENT	64  extern __pdata angle_t	ao_sample_orient; +extern __pdata angle_t	ao_sample_orients[AO_NUM_ORIENT]; +extern __pdata uint8_t	ao_sample_orient_pos;  #endif  void ao_sample_init(void); diff --git a/src/kernel/ao_usb.h b/src/kernel/ao_usb.h index 936d939b..40516de1 100644 --- a/src/kernel/ao_usb.h +++ b/src/kernel/ao_usb.h @@ -41,7 +41,23 @@ ao_usb_pollchar(void);  void  ao_usb_flush(void); +#if AO_USB_HAS_IN2 +void +ao_usb_flush2(void); + +void +ao_usb_putchar2(char c); +#endif + +#if AO_USB_HAS_IN3 +void +ao_usb_flush3(void); + +void +ao_usb_putchar3(char c); +#endif  /* Enable the USB controller */ +  void  ao_usb_enable(void); @@ -107,6 +123,7 @@ extern __code __at (0x00aa) uint8_t ao_usb_descriptors [];  #define AO_USB_OUT_EP		4  #define AO_USB_IN_EP		5  #define AO_USB_IN2_EP		6 +#define AO_USB_IN3_EP		7  #endif  #ifndef AO_USB_HAS_OUT @@ -125,6 +142,10 @@ extern __code __at (0x00aa) uint8_t ao_usb_descriptors [];  #define AO_USB_HAS_IN2	0  #endif +#ifndef AO_USB_HAS_IN3 +#define AO_USB_HAS_IN3	0 +#endif +  /*   * USB bulk packets can only come in 8, 16, 32 and 64   * byte sizes, so we'll use 64 for everything  | 
