![](/media/cache/profiles/8158fa3e4de806e614f7ff02e7b22fde.jpg.50x50_q85.png)
New version of quadcopter software written to OO principles
Dependencies: mbed MODSERIAL filter mbed-rtos ConfigFile PID PPM FreeIMU_external_magnetometer TinyGPS
Diff: Sensors/Sensors.cpp
- Revision:
- 2:969dfa4f2436
- Parent:
- 0:c6a85bb2a827
- Child:
- 3:4823d6750629
diff -r ec3521d90369 -r 969dfa4f2436 Sensors/Sensors.cpp --- a/Sensors/Sensors.cpp Wed Mar 04 18:53:43 2015 +0000 +++ b/Sensors/Sensors.cpp Wed Apr 01 11:19:21 2015 +0000 @@ -0,0 +1,160 @@ +#include "Sensors.h" + +Sensors::Sensors(Status& status, ConfigFileWrapper& configFileWrapper, PinName gpsPinTx, PinName gpsPinRx, PinName i2cSda, PinName i2cScl, PinName lidarInterrupt) : _status(status) +{ + _gpsValues = Gps::Value(); + _position = Position(); + _altitude = Altitude(); + + //Initialise IMU + _imu = new Imu(configFileWrapper); + _imu->zeroGyro(); + + //Initialise GPS + _gps = new Gps(gpsPinTx, gpsPinRx); + + //Initialise Lidar + _lidar = new LidarLitePwm(lidarInterrupt); + + //Initialise kalman + _altitudeKalmanFilter = new Kalman(0.75, 2, 1, 0); + + DEBUG("Sensors initialised\r\n"); +} + +Sensors::~Sensors(){} + +void Sensors::update() +{ + //Update GPS + updateGpsValues(); + + //Update Altitude + updateAltitude(); + + //updatePosition(); +} + +Imu::Rate Sensors::getRate() +{ + return _rate; +} + +Imu::Angle Sensors::getAngle() +{ + return _angle; +} + +Gps::Value Sensors::getGpsValues() +{ + return _gpsValues; +} + +Sensors::Altitude Sensors::getAltitude() +{ + return _altitude; +} + +Sensors::Position Sensors::getPosition() +{ + return _position; +} + +double Sensors::getZVelocity() +{ + return _imu->getVelocity(); +} + +void Sensors::updateImu() +{ + _angle = _imu->getAngle(); + _rate = _imu->getRate(); + + return; +} + +void Sensors::updateGpsValues() +{ + _gpsValues = _gps->getValues(); +} + +void Sensors::updateAltitude() +{ + _altitude.lidar = getLidarAltitude(); //cm + _altitude.barometer = _imu->getAltitude(); //cm + _altitude.gps = _gpsValues.altitude; //m + + //Update IMU velocity + double time = (1.0 / ((double)FLIGHT_CONTROLLER_FREQUENCY / 10.00)); // In seconds + double velocity = _imu->getVelocity(time); + + //Compute predicted altitude + double predictedAltitude = _altitude.computed + velocity; + + //Compute predicted change in altitude + double predictedChange = 1; + if(_altitude.computed != 0) predictedChange = predictedAltitude / _altitude.computed; + + //Compute estimated altitude + double estimatedAltitude = _altitudeKalmanFilter->update(predictedChange, _altitude.lidar); + + //Compute estimated velocity + double estimatedVelocity = estimatedAltitude - _altitude.computed; + + //Reset IMU velocity to estimated velocity + _imu->setCurrentVelocity(estimatedVelocity); + + //Save new altitude + _altitude.computed = estimatedAltitude; + + //printf("%1.6f, %1.6f, %1.6f\r\n", predictedAltitude, _altitude.lidar, _altitude.computed); +} + + +void Sensors::updatePosition() +{ + +} + +void Sensors::zeroGyro() +{ + _imu->zeroGyro(); +} + +void Sensors::zeroBarometer() +{ + _imu->zeroBarometer(); +} + +void Sensors::enable(bool enable) +{ + _imu->enable(enable); +} + +int Sensors::getLidarAltitude() +{ + Imu::Angle angles = getAngle(); + int rawAltitude = _lidar->read(); + + double oppAng = 0; + double multiplier = 0; + int pitchAltitude = 0; + int rollAltitude = 0; + + //Calulate pitch altitude + oppAng = 90 - abs(angles.pitch); + multiplier = sin(oppAng*PI/180); + pitchAltitude = multiplier * rawAltitude; + + //Calulate roll altitude + oppAng = 90 - abs(angles.roll); + multiplier = sin(oppAng*PI/180); + rollAltitude = multiplier * rawAltitude; + + return (pitchAltitude + rollAltitude)/ 2; +} + +void Sensors::zeroAccel() +{ + _imu->zeroAccel(); +} \ No newline at end of file