mirror of https://github.com/ArduPilot/ardupilot
AP_HAL_SITL: ADC resolution configurable by define, default to 16 bit
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0b34df3328
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4ef070956d
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@ -5,6 +5,8 @@
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#include "AnalogIn.h"
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#include "AnalogIn.h"
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#include <stdint.h>
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#include <stdint.h>
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#define VOLTAGE_TO_PIN_VALUE(_v) (constrain_float(_v * (SITL_ADC_MAX_PIN_VALUE/SITL_ADC_FULL_SCALE_VOLTAGE), 0, SITL_ADC_MAX_PIN_VALUE))
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using namespace HALSITL;
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using namespace HALSITL;
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extern const AP_HAL::HAL& hal;
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extern const AP_HAL::HAL& hal;
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@ -19,38 +21,34 @@ float ADCSource::read_average() {
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}
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}
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float ADCSource::voltage_average() {
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float ADCSource::voltage_average() {
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return (5.0f/1023.0f) * read_average();
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return voltage_latest();
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}
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}
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float ADCSource::voltage_latest() {
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float ADCSource::voltage_latest() {
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return (5.0f/1023.0f) * read_latest();
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}
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float ADCSource::read_latest() {
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switch (_pin) {
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switch (_pin) {
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case ANALOG_INPUT_BOARD_VCC:
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case ANALOG_INPUT_BOARD_VCC:
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return 1023;
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return SITL_ADC_MAX_PIN_VALUE;
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case 0:
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case 0:
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return _sitlState->sonar_pin_value;
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return _sitlState->sonar_pin_voltage;
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case 1:
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case 1:
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return _sitlState->airspeed_pin_value[0];
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return _sitlState->airspeed_pin_voltage[0];
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case 2:
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case 2:
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return _sitlState->airspeed_pin_value[1];
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return _sitlState->airspeed_pin_voltage[1];
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case 12:
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case 12:
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return _sitlState->current_pin_value;
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return _sitlState->current_pin_voltage;
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case 13:
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case 13:
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return _sitlState->voltage_pin_value;
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return _sitlState->voltage_pin_voltage;
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case 14:
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case 14:
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return _sitlState->current2_pin_value;
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return _sitlState->current2_pin_voltage;
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case 15:
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case 15:
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return _sitlState->voltage2_pin_value;
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return _sitlState->voltage2_pin_voltage;
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case ANALOG_INPUT_NONE:
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case ANALOG_INPUT_NONE:
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default:
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default:
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@ -58,6 +56,10 @@ float ADCSource::read_latest() {
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}
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}
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}
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}
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float ADCSource::read_latest() {
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return VOLTAGE_TO_PIN_VALUE(voltage_latest());
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}
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bool ADCSource::set_pin(uint8_t pin) {
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bool ADCSource::set_pin(uint8_t pin) {
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_pin = pin;
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_pin = pin;
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return true;
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return true;
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@ -3,6 +3,9 @@
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#include <AP_HAL/AP_HAL.h>
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#include <AP_HAL/AP_HAL.h>
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#include "AP_HAL_SITL_Namespace.h"
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#include "AP_HAL_SITL_Namespace.h"
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#define SITL_ADC_RESOLUTION 16 // bits of resolution
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#define SITL_ADC_MAX_PIN_VALUE ((1<<SITL_ADC_RESOLUTION)-1)
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#define SITL_ADC_FULL_SCALE_VOLTAGE 5.0f
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#define SITL_INPUT_MAX_CHANNELS 12
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#define SITL_INPUT_MAX_CHANNELS 12
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class HALSITL::ADCSource : public AP_HAL::AnalogSource {
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class HALSITL::ADCSource : public AP_HAL::AnalogSource {
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@ -912,11 +912,11 @@ void SITL_State::_simulator_servos(struct sitl_input &input)
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}
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}
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// assume 3DR power brick
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// assume 3DR power brick
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voltage_pin_value = float_to_uint16(((voltage / 10.1f) / 5.0f) * 1024);
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voltage_pin_voltage = (voltage / 10.1f);
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current_pin_value = float_to_uint16(((_current / 17.0f) / 5.0f) * 1024);
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current_pin_voltage = _current/17.0f;
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// fake battery2 as just a 25% gain on the first one
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// fake battery2 as just a 25% gain on the first one
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voltage2_pin_value = float_to_uint16(((voltage * 0.25f / 10.1f) / 5.0f) * 1024);
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voltage2_pin_voltage = voltage_pin_voltage * .25f;
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current2_pin_value = float_to_uint16(((_current * 0.25f / 17.0f) / 5.0f) * 1024);
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current2_pin_voltage = current_pin_voltage * .25f;
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}
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}
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void SITL_State::init(int argc, char * const argv[])
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void SITL_State::init(int argc, char * const argv[])
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@ -96,12 +96,12 @@ public:
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}
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}
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// simulated airspeed, sonar and battery monitor
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// simulated airspeed, sonar and battery monitor
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uint16_t sonar_pin_value; // pin 0
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float sonar_pin_voltage; // pin 0
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uint16_t airspeed_pin_value[AIRSPEED_MAX_SENSORS]; // pin 1
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float airspeed_pin_voltage[AIRSPEED_MAX_SENSORS]; // pin 1
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uint16_t voltage_pin_value; // pin 13
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float voltage_pin_voltage; // pin 13
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uint16_t current_pin_value; // pin 12
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float current_pin_voltage; // pin 12
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uint16_t voltage2_pin_value; // pin 15
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float voltage2_pin_voltage; // pin 15
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uint16_t current2_pin_value; // pin 14
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float current2_pin_voltage; // pin 14
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// paths for UART devices
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// paths for UART devices
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const char *_uart_path[9] {
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const char *_uart_path[9] {
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@ -20,6 +20,10 @@ extern const AP_HAL::HAL& hal;
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using namespace HALSITL;
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using namespace HALSITL;
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// scaling value taken from AP_Airspeed_analog.cpp
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#define VOLTS_TO_PASCAL 819
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#define PASCAL_TO_VOLTS(_p) (_p/VOLTS_TO_PASCAL)
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// return current scale factor that converts from equivalent to true airspeed
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// return current scale factor that converts from equivalent to true airspeed
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// valid for altitudes up to 10km AMSL
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// valid for altitudes up to 10km AMSL
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// assumes standard atmosphere lapse rate
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// assumes standard atmosphere lapse rate
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@ -79,7 +83,7 @@ void SITL_State::_update_airspeed(float true_airspeed)
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_sitl->state.airspeed_raw_pressure[i] = airspeed_pressure;
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_sitl->state.airspeed_raw_pressure[i] = airspeed_pressure;
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airspeed_pin_value[i] = MIN(0xFFFF, airspeed_raw / 4);
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airspeed_pin_voltage[i] = PASCAL_TO_VOLTS(airspeed_raw);
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}
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}
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}
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}
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@ -51,7 +51,7 @@ float SITL_State::_sonar_pin_voltage() const
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*/
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*/
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void SITL_State::_update_rangefinder()
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void SITL_State::_update_rangefinder()
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{
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{
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sonar_pin_value = 1023 * (_sonar_pin_voltage() / 5.0f);
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sonar_pin_voltage = _sonar_pin_voltage();
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}
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}
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#endif
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#endif
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