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AP_InertialSensor: removed unused new_data_available() and temperature() APIs

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This commit is contained in:
Andrew Tridgell 2013-02-07 10:23:37 +11:00
parent 7b1245937c
commit 5643c371b9
9 changed files with 4 additions and 47 deletions
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6
libraries/AP_InertialSensor/AP_InertialSensor.h
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@ -104,12 +104,6 @@ public:
*/
virtual bool update() = 0;
// check if the sensors have new data
virtual bool new_data_available(void) = 0;
/* Temperature, in degrees celsius, of the gyro. */
virtual float temperature() = 0;
/* get_delta_time returns the time period in seconds
* overwhich the sensor data was collected
*/

9
libraries/AP_InertialSensor/AP_InertialSensor_Oilpan.cpp
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@ -107,15 +107,6 @@ bool AP_InertialSensor_Oilpan::update()
return true;
}
bool AP_InertialSensor_Oilpan::new_data_available( void )
{
return _adc->new_data_available(_sensors);
}
float AP_InertialSensor_Oilpan::temperature() {
return _temp;
}
float AP_InertialSensor_Oilpan::get_delta_time() {
return _delta_time_micros * 1.0e-6;
}

2
libraries/AP_InertialSensor/AP_InertialSensor_Oilpan.h
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@ -17,8 +17,6 @@ public:
/* Concrete implementation of AP_InertialSensor functions: */
bool update();
bool new_data_available();
float temperature();
float get_delta_time(); // get_delta_time returns the time period in seconds overwhich the sensor data was collected
//uint32_t get_last_sample_time_micros(); // last_sample_time - get time (in microseconds) that last sample was captured
float get_gyro_drift_rate();

11
libraries/AP_InertialSensor/AP_InertialSensor_PX4.cpp
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@ -109,17 +109,6 @@ bool AP_InertialSensor_PX4::update(void)
return true;
}
bool AP_InertialSensor_PX4::new_data_available(void)
{
return num_samples_available() > 0;
}
float AP_InertialSensor_PX4::temperature(void)
{
return 0.0;
}
float AP_InertialSensor_PX4::get_delta_time(void)
{
return _delta_time;

2
libraries/AP_InertialSensor/AP_InertialSensor_PX4.h
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@ -21,8 +21,6 @@ public:
/* Concrete implementation of AP_InertialSensor functions: */
bool update();
bool new_data_available();
float temperature();
float get_delta_time();
uint32_t get_last_sample_time_micros();
float get_gyro_drift_rate();

7
libraries/AP_InertialSensor/AP_InertialSensor_Stub.cpp
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@ -27,14 +27,7 @@ bool AP_InertialSensor_Stub::update( void ) {
_last_update_ms = now;
return true;
}
bool AP_InertialSensor_Stub::new_data_available( void ) {
return num_samples_available() > 0;
}
float AP_InertialSensor_Stub::temperature() {
return 0.0;
}
float AP_InertialSensor_Stub::get_delta_time() {
return _delta_time_usec * 1.0e-6;
}

2
libraries/AP_InertialSensor/AP_InertialSensor_Stub.h
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@ -15,8 +15,6 @@ public:
/* Concrete implementation of AP_InertialSensor functions: */
bool update();
bool new_data_available();
float temperature();
float get_delta_time();
uint32_t get_last_sample_time_micros();
float get_gyro_drift_rate();

6
libraries/AP_InertialSensor/examples/MPU6000/MPU6000.pde
View File

@ -169,7 +169,6 @@ void run_test()
{
Vector3f accel;
Vector3f gyro;
float temperature;
float length;
uint8_t counter = 0;
@ -191,14 +190,13 @@ void run_test()
ins.update();
accel = ins.get_accel();
gyro = ins.get_gyro();
temperature = ins.temperature();
length = accel.length();
if (counter++ % 50 == 0) {
// display results
hal.console->printf_P(PSTR("Accel X:%4.2f \t Y:%4.2f \t Z:%4.2f \t len:%4.2f \t Gyro X:%4.2f \t Y:%4.2f \t Z:%4.2f \t Temp:%4.2f\n"),
accel.x, accel.y, accel.z, length, gyro.x, gyro.y, gyro.z, temperature);
hal.console->printf_P(PSTR("Accel X:%4.2f \t Y:%4.2f \t Z:%4.2f \t len:%4.2f \t Gyro X:%4.2f \t Y:%4.2f \t Z:%4.2f\n"),
accel.x, accel.y, accel.z, length, gyro.x, gyro.y, gyro.z);
}
}

6
libraries/AP_InertialSensor/examples/PX4/PX4.pde
View File

@ -151,7 +151,6 @@ void run_test()
{
Vector3f accel;
Vector3f gyro;
float temperature;
float length;
uint8_t counter = 0;
@ -175,14 +174,13 @@ void run_test()
ins.update();
accel = ins.get_accel();
gyro = ins.get_gyro();
temperature = ins.temperature();
length = accel.length();
if (counter++ % 50 == 0) {
// display results
hal.console->printf_P(PSTR("Accel X:%4.2f \t Y:%4.2f \t Z:%4.2f \t len:%4.2f \t Gyro X:%4.2f \t Y:%4.2f \t Z:%4.2f \t Temp:%4.2f dt:%u\n"),
accel.x, accel.y, accel.z, length, gyro.x, gyro.y, gyro.z, temperature,
hal.console->printf_P(PSTR("Accel X:%4.2f \t Y:%4.2f \t Z:%4.2f \t len:%4.2f \t Gyro X:%4.2f \t Y:%4.2f \t Z:%4.2f \t dt:%u\n"),
accel.x, accel.y, accel.z, length, gyro.x, gyro.y, gyro.z,
(unsigned)(1.0e6*ins.get_delta_time()));
}
}