/*
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 3 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.
You should have received a copy of the GNU General Public License
along with this program. If not, see .
*/
/*
backend driver for airspeed from a I2C MS5525D0 sensor
*/
#include "AP_Airspeed_MS5525.h"
#include
#include
#include
#include
#include
#include
#include
#include
extern const AP_HAL::HAL &hal;
#define MS5525D0_I2C_ADDR_1 0x76
#define MS5525D0_I2C_ADDR_2 0x77
#define REG_RESET 0x1E
#define REG_CONVERT_D1_OSR_256 0x40
#define REG_CONVERT_D1_OSR_512 0x42
#define REG_CONVERT_D1_OSR_1024 0x44
#define REG_CONVERT_D1_OSR_2048 0x46
#define REG_CONVERT_D1_OSR_4096 0x48
#define REG_CONVERT_D2_OSR_256 0x50
#define REG_CONVERT_D2_OSR_512 0x52
#define REG_CONVERT_D2_OSR_1024 0x54
#define REG_CONVERT_D2_OSR_2048 0x56
#define REG_CONVERT_D2_OSR_4096 0x58
#define REG_ADC_READ 0x00
#define REG_PROM_BASE 0xA0
// go for 1024 oversampling. This should be fast enough to reduce
// noise but low enough to keep self-heating small
#define REG_CONVERT_PRESSURE REG_CONVERT_D1_OSR_1024
#define REG_CONVERT_TEMPERATURE REG_CONVERT_D2_OSR_1024
AP_Airspeed_MS5525::AP_Airspeed_MS5525(AP_Airspeed &_frontend, uint8_t _instance, MS5525_ADDR address) :
AP_Airspeed_Backend(_frontend, _instance)
{
_address = address;
}
// probe and initialise the sensor
bool AP_Airspeed_MS5525::init()
{
const uint8_t addresses[] = { MS5525D0_I2C_ADDR_1, MS5525D0_I2C_ADDR_2 };
bool found = false;
for (uint8_t i=0; iget_device(get_bus(), addresses[i]);
if (!dev) {
continue;
}
if (!dev->get_semaphore()->take(HAL_SEMAPHORE_BLOCK_FOREVER)) {
continue;
}
// lots of retries during probe
dev->set_retries(5);
found = read_prom();
if (found) {
printf("MS5525: Found sensor on bus %u address 0x%02x\n", get_bus(), addresses[i]);
break;
}
dev->get_semaphore()->give();
}
if (!found) {
printf("MS5525: no sensor found\n");
return false;
}
// Send a command to read temperature first
uint8_t reg = REG_CONVERT_TEMPERATURE;
dev->transfer(®, 1, nullptr, 0);
state = 0;
command_send_us = AP_HAL::micros();
// drop to 2 retries for runtime
dev->set_retries(2);
dev->get_semaphore()->give();
// read at 80Hz
dev->register_periodic_callback(1000000UL/80U,
FUNCTOR_BIND_MEMBER(&AP_Airspeed_MS5525::timer, void));
return true;
}
/**
* CRC used by MS pressure devices
*/
uint16_t AP_Airspeed_MS5525::crc4_prom(void)
{
return crc_crc4(prom);
}
bool AP_Airspeed_MS5525::read_prom(void)
{
// reset the chip to ensure it has correct prom values loaded
uint8_t reg = REG_RESET;
if (!dev->transfer(®, 1, nullptr, 0)) {
return false;
}
hal.scheduler->delay(5);
bool all_zero = true;
for (uint8_t i = 0; i < 8; i++) {
be16_t val;
if (!dev->read_registers(REG_PROM_BASE+i*2, (uint8_t *) &val,
sizeof(uint16_t))) {
return false;
}
prom[i] = be16toh(val);
if (prom[i] != 0) {
all_zero = false;
}
}
if (all_zero) {
return false;
}
/* save the read crc */
const uint16_t crc_read = prom[7] & 0xf;
/* remove CRC byte */
prom[7] &= 0xff00;
uint16_t crc_calc = crc4_prom();
if (crc_read != crc_calc) {
printf("MS5525: CRC mismatch 0x%04x 0x%04x\n", crc_read, crc_calc);
}
return crc_read == crc_calc;
}
/*
read from the ADC
*/
int32_t AP_Airspeed_MS5525::read_adc()
{
uint8_t val[3];
if (!dev->read_registers(REG_ADC_READ, val, 3)) {
return 0;
}
return (val[0] << 16) | (val[1] << 8) | val[2];
}
/*
calculate pressure and temperature
*/
void AP_Airspeed_MS5525::calculate(void)
{
// table for the 001DS part, 1PSI range
const uint8_t Q1 = 15;
const uint8_t Q2 = 17;
const uint8_t Q3 = 7;
const uint8_t Q4 = 5;
const uint8_t Q5 = 7;
const uint8_t Q6 = 21;
int64_t dT = D2 - int64_t(prom[5]) * (1UL<transfer(&cmd_sent, 1, nullptr, 0)) {
command_send_us = AP_HAL::micros();
}
// when we get adc_val == 0 then then both the current value and
// the next value we read from the sensor are invalid
ignore_next = true;
return;
}
/*
* If read fails, re-initiate a read command for current state or we are
* stuck
*/
if (!ignore_next) {
if (cmd_sent == REG_CONVERT_TEMPERATURE) {
D2 = adc_val;
} else if (cmd_sent == REG_CONVERT_PRESSURE) {
D1 = adc_val;
calculate();
}
}
ignore_next = false;
cmd_sent = (state == 0) ? REG_CONVERT_TEMPERATURE : REG_CONVERT_PRESSURE;
if (!dev->transfer(&cmd_sent, 1, nullptr, 0)) {
// we don't know for sure what state the sensor is in when we
// fail to send the command, so ignore the next response
ignore_next = true;
return;
}
command_send_us = AP_HAL::micros();
state = (state + 1) % 5;
}
// return the current differential_pressure in Pascal
bool AP_Airspeed_MS5525::get_differential_pressure(float &_pressure)
{
if ((AP_HAL::millis() - last_sample_time_ms) > 100) {
return false;
}
WITH_SEMAPHORE(sem);
if (press_count > 0) {
pressure = pressure_sum / press_count;
press_count = 0;
pressure_sum = 0;
}
_pressure = pressure;
return true;
}
// return the current temperature in degrees C, if available
bool AP_Airspeed_MS5525::get_temperature(float &_temperature)
{
if ((AP_HAL::millis() - last_sample_time_ms) > 100) {
return false;
}
WITH_SEMAPHORE(sem);
if (temp_count > 0) {
temperature = temperature_sum / temp_count;
temp_count = 0;
temperature_sum = 0;
}
_temperature = temperature;
return true;
}