mirror of https://github.com/ArduPilot/ardupilot
AP_Airspeed: added ASP5033 driver
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@ -31,6 +31,7 @@
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#include "AP_Airspeed_SDP3X.h"
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#include "AP_Airspeed_DLVR.h"
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#include "AP_Airspeed_analog.h"
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#include "AP_Airspeed_ASP5033.h"
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#include "AP_Airspeed_Backend.h"
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#if HAL_ENABLE_LIBUAVCAN_DRIVERS
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#include "AP_Airspeed_UAVCAN.h"
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@ -83,7 +84,7 @@ const AP_Param::GroupInfo AP_Airspeed::var_info[] = {
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// @Param: _TYPE
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// @DisplayName: Airspeed type
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// @Description: Type of airspeed sensor
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// @Values: 0:None,1:I2C-MS4525D0,2:Analog,3:I2C-MS5525,4:I2C-MS5525 (0x76),5:I2C-MS5525 (0x77),6:I2C-SDP3X,7:I2C-DLVR-5in,8:UAVCAN,9:I2C-DLVR-10in,10:I2C-DLVR-20in,11:I2C-DLVR-30in,12:I2C-DLVR-60in,13:NMEA water speed,14:MSP
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// @Values: 0:None,1:I2C-MS4525D0,2:Analog,3:I2C-MS5525,4:I2C-MS5525 (0x76),5:I2C-MS5525 (0x77),6:I2C-SDP3X,7:I2C-DLVR-5in,8:UAVCAN,9:I2C-DLVR-10in,10:I2C-DLVR-20in,11:I2C-DLVR-30in,12:I2C-DLVR-60in,13:NMEA water speed,14:MSP,15:ASP5033
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// @User: Standard
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AP_GROUPINFO_FLAGS("_TYPE", 0, AP_Airspeed, param[0].type, ARSPD_DEFAULT_TYPE, AP_PARAM_FLAG_ENABLE),
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@ -190,7 +191,7 @@ const AP_Param::GroupInfo AP_Airspeed::var_info[] = {
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// @Param: 2_TYPE
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// @DisplayName: Second Airspeed type
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// @Description: Type of 2nd airspeed sensor
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// @Values: 0:None,1:I2C-MS4525D0,2:Analog,3:I2C-MS5525,4:I2C-MS5525 (0x76),5:I2C-MS5525 (0x77),6:I2C-SDP3X,7:I2C-DLVR-5in,8:UAVCAN,9:I2C-DLVR-10in,10:I2C-DLVR-20in,11:I2C-DLVR-30in,12:I2C-DLVR-60in,13:NMEA water speed,14:MSP
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// @Values: 0:None,1:I2C-MS4525D0,2:Analog,3:I2C-MS5525,4:I2C-MS5525 (0x76),5:I2C-MS5525 (0x77),6:I2C-SDP3X,7:I2C-DLVR-5in,8:UAVCAN,9:I2C-DLVR-10in,10:I2C-DLVR-20in,11:I2C-DLVR-30in,12:I2C-DLVR-60in,13:NMEA water speed,14:MSP,15:ASP5033
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// @User: Standard
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AP_GROUPINFO_FLAGS("2_TYPE", 11, AP_Airspeed, param[1].type, 0, AP_PARAM_FLAG_ENABLE),
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@ -354,6 +355,11 @@ void AP_Airspeed::init()
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case TYPE_I2C_DLVR_60IN:
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#if !HAL_MINIMIZE_FEATURES
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sensor[i] = new AP_Airspeed_DLVR(*this, i, 60);
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#endif // !HAL_MINIMIZE_FEATURES
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break;
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case TYPE_I2C_ASP5033:
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#if !HAL_MINIMIZE_FEATURES
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sensor[i] = new AP_Airspeed_ASP5033(*this, i);
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#endif // !HAL_MINIMIZE_FEATURES
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break;
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case TYPE_UAVCAN:
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@ -167,6 +167,7 @@ public:
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TYPE_I2C_DLVR_60IN=12,
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TYPE_NMEA_WATER=13,
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TYPE_MSP=14,
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TYPE_I2C_ASP5033=15,
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};
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// get current primary sensor
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@ -0,0 +1,173 @@
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/*
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This program is free software: you can redistribute it and/or modify
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it under the terms of the GNU General Public License as published by
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the Free Software Foundation, either version 3 of the License, or
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(at your option) any later version.
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This program is distributed in the hope that it will be useful,
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but WITHOUT ANY WARRANTY; without even the implied warranty of
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MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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GNU General Public License for more details.
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You should have received a copy of the GNU General Public License
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along with this program. If not, see <http://www.gnu.org/licenses/>.
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*/
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/*
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backend driver for airspeed sensor from www.qio-tek.com
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I2C ASP5033 sensor
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*/
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#include "AP_Airspeed_ASP5033.h"
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#include <AP_HAL/I2CDevice.h>
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extern const AP_HAL::HAL &hal;
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#define ASP5033_I2C_ADDR_1 0x6C
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#define ASP5033_I2C_ADDR_2 0x6D
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#define REG_CMD 0x30
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#define REG_PRESS_DATA 0x06
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#define REG_TEMP_DATA 0x09
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#define REG_PART_ID 0x01
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#define REG_PART_ID_SET 0xa4
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#define REG_SENSOR_READY 0x08
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#define REG_WHOAMI_DEFAULT_ID 0X00
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#define REG_WHOAMI_RECHECK_ID 0X66
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#define CMD_MEASURE 0x0A
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bool AP_Airspeed_ASP5033::init()
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{
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// probe the sensor, supporting multiple possible I2C addresses
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const uint8_t addresses[] = { ASP5033_I2C_ADDR_1, ASP5033_I2C_ADDR_2 };
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for (uint8_t address : addresses) {
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dev = hal.i2c_mgr->get_device(get_bus(), address);
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if (!dev) {
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continue;
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}
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WITH_SEMAPHORE(dev->get_semaphore());
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dev->set_speed(AP_HAL::Device::SPEED_HIGH);
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dev->set_retries(2);
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if (!confirm_sensor_id()) {
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continue;
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}
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dev->register_periodic_callback(1000000UL/80U,
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FUNCTOR_BIND_MEMBER(&AP_Airspeed_ASP5033::timer, void));
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return true;
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}
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// not found
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return false;
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}
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/*
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this sensor has an unusual whoami scheme. The part_id is changeable
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via another register. We check the sensor by looking for the
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expected behaviour
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*/
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bool AP_Airspeed_ASP5033::confirm_sensor_id(void)
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{
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uint8_t part_id;
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if (!dev->read_registers(REG_PART_ID_SET, &part_id, 1) ||
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part_id != REG_WHOAMI_DEFAULT_ID) {
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return false;
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}
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if (!dev->write_register(REG_PART_ID_SET, REG_WHOAMI_RECHECK_ID)) {
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return false;
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}
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if (!dev->read_registers(REG_PART_ID, &part_id, 1) ||
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part_id != REG_WHOAMI_RECHECK_ID) {
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return false;
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}
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return true;
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}
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// read the data from the sensor
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void AP_Airspeed_ASP5033::timer()
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{
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// request a new measurement cycle begin
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dev->write_register(REG_CMD, CMD_MEASURE);
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uint8_t status;
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if (!dev->read_registers(REG_CMD, &status, 1) ||
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(status & REG_SENSOR_READY) == 0) {
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// no data ready
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return;
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}
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// read pressure and temperature as one block
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uint8_t data[5];
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if (!dev->read_registers(REG_PRESS_DATA, data, sizeof(data))) {
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return;
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}
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// ADC pressure is signed 24 bit
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int32_t press = (data[0]<<24) | (data[1]<<16) | (data[2]<<8);
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// convert back to 24 bit
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press >>= 8;
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// k is a shift based on the pressure range of the device. See
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// table in the datasheet
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constexpr uint8_t k = 7;
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constexpr float press_scale = 1.0 / (1U<<k);
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// temperature is 16 bit signed in units of 1/256 C
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const int16_t temp = (data[3]<<8) | data[4];
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constexpr float temp_scale = 1.0 / 256;
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WITH_SEMAPHORE(sem);
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press_sum += press * press_scale;
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temp_sum += temp * temp_scale;
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press_count++;
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temp_count++;
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last_sample_ms = AP_HAL::millis();
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}
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// return the current differential_pressure in Pascal
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bool AP_Airspeed_ASP5033::get_differential_pressure(float &pressure)
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{
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WITH_SEMAPHORE(sem);
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if (AP_HAL::millis() - last_sample_ms > 100) {
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return false;
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}
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if (press_count == 0) {
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pressure = last_pressure;
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return true;
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}
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last_pressure = pressure = press_sum / press_count;
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press_count = 0;
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press_sum = 0;
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return true;
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}
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// return the current temperature in degrees C, if available
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bool AP_Airspeed_ASP5033::get_temperature(float &temperature)
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{
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WITH_SEMAPHORE(sem);
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if (AP_HAL::millis() - last_sample_ms > 100) {
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return false;
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}
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if (temp_count == 0) {
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temperature = last_temperature;
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return true;
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}
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last_temperature = temperature = temp_sum / temp_count;
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temp_count = 0;
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temp_sum = 0;
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return true;
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}
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@ -0,0 +1,46 @@
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/*
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This program is free software: you can redistribute it and/or modify
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it under the terms of the GNU General Public License as published by
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the Free Software Foundation, either version 3 of the License, or
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(at your option) any later version.
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This program is distributed in the hope that it will be useful,
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but WITHOUT ANY WARRANTY; without even the implied warranty of
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MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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GNU General Public License for more details.
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You should have received a copy of the GNU General Public License
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along with this program. If not, see <http://www.gnu.org/licenses/>.
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*/
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#pragma once
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/*
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backend driver for airspeed from I2C
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*/
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#include "AP_Airspeed_Backend.h"
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class AP_Airspeed_ASP5033 : public AP_Airspeed_Backend
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{
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public:
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using AP_Airspeed_Backend::AP_Airspeed_Backend;
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bool init() override;
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// return the current differential_pressure in Pascal
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bool get_differential_pressure(float &_pressure) override;
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// return the current temperature in degrees C, if available
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bool get_temperature(float &_temperature) override;
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private:
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void timer();
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bool confirm_sensor_id(void);
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float temp_sum;
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float press_sum;
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float last_pressure;
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float last_temperature;
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uint32_t press_count;
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uint32_t temp_count;
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uint32_t last_sample_ms;
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AP_HAL::OwnPtr<AP_HAL::I2CDevice> dev;
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};
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