ardupilot/libraries/APO/AP_Navigator.h

298 lines
6.5 KiB
C++

/*
* AP_Navigator.h
* Copyright (C) James Goppert 2010 <james.goppert@gmail.com>
*
* This file 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 file 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 <http://www.gnu.org/licenses/>.
*/
#ifndef AP_Navigator_H
#define AP_Navigator_H
#include "constants.h"
#include <inttypes.h>
namespace apo {
class AP_Board;
/// Navigator class
class AP_Navigator {
public:
AP_Navigator(AP_Board * board);
// note, override these with derived navigator functionality
virtual void calibrate() {};
virtual void updateFast(float dt) {};
virtual void updateSlow(float dt) {};
// accessors
float getPD() const;
float getPE() const;
float getPN() const;
void setPD(float _pD);
void setPE(float _pE);
void setPN(float _pN);
float getAirSpeed() const {
// neglects vertical wind
float vWN = getVN() + getWindSpeed()*cos(getWindDirection());
float vWE = getVE() + getWindSpeed()*sin(getWindDirection());
return sqrt(vWN*vWN+vWE+vWE+getVD()*getVD());
}
float getGroundSpeed() const {
return sqrt(getVN()*getVN()+getVE()*getVE());
}
float getWindSpeed() const {
return _windSpeed;
}
int32_t getAlt_intM() const {
return _alt_intM;
}
float getAlt() const {
return _alt_intM / scale_m;
}
void setAlt(float _alt) {
this->_alt_intM = _alt * scale_m;
}
float getLat() const {
//Serial.print("getLatfirst");
//Serial.println(_lat_degInt * degInt2Rad);
return _lat_degInt * degInt2Rad;
}
void setLat(float _lat) {
//Serial.print("setLatfirst");
//Serial.println(_lat * rad2DegInt);
setLat_degInt(_lat*rad2DegInt);
}
float getLon() const {
return _lon_degInt * degInt2Rad;
}
void setLon(float _lon) {
this->_lon_degInt = _lon * rad2DegInt;
}
float getVN() const {
return _vN;
}
float getVE() const {
return _vE;
}
float getVD() const {
return _vD;
}
int32_t getLat_degInt() const {
//Serial.print("getLat_degInt");
//Serial.println(_lat_degInt);
return _lat_degInt;
}
int32_t getLon_degInt() const {
return _lon_degInt;
}
float getPitch() const {
return _pitch;
}
float getPitchRate() const {
return _pitchRate;
}
float getRoll() const {
return _roll;
}
float getRollRate() const {
return _rollRate;
}
float getYaw() const {
return _yaw;
}
float getYawRate() const {
return _yawRate;
}
float getWindDirection() const {
return _windDirection;
}
float getCourseOverGround() const {
return atan2(getVE(),getVN());
}
float getRelativeCourseOverGround() const {
float y = getCourseOverGround() - getYaw();
if (y > 180 * deg2Rad)
y -= 360 * deg2Rad;
if (y < -180 * deg2Rad)
y += 360 * deg2Rad;
return y;
}
float getSpeedOverGround() const {
return sqrt(getVN()*getVN()+getVE()*getVE());
}
float getXAccel() const {
return _xAccel;
}
float getYAccel() const {
return _yAccel;
}
float getZAccel() const {
return _zAccel;
}
void setAirSpeed(float airSpeed) {
// assumes wind constant and rescale navigation speed
float vScale = (1 + airSpeed/getAirSpeed());
float vNorm = sqrt(getVN()*getVN()+getVE()*getVE()+getVD()*getVD());
_vN *= vScale/vNorm;
_vE *= vScale/vNorm;
_vD *= vScale/vNorm;
}
void setAlt_intM(int32_t alt_intM) {
_alt_intM = alt_intM;
}
void setVN(float vN) {
_vN = vN;
}
void setVE(float vE) {
_vE = vE;
}
void setVD(float vD) {
_vD = vD;
}
void setXAccel(float xAccel) {
_xAccel = xAccel;
}
void setYAccel(float yAccel) {
_yAccel = yAccel;
}
void setZAccel(float zAccel) {
_zAccel = zAccel;
}
void setGroundSpeed(float groundSpeed) {
float cog = getCourseOverGround();
_vN = cos(cog)*groundSpeed;
_vE = sin(cog)*groundSpeed;
}
void setLat_degInt(int32_t lat_degInt) {
_lat_degInt = lat_degInt;
//Serial.print("setLat_degInt");
//Serial.println(_lat_degInt);
}
void setLon_degInt(int32_t lon_degInt) {
_lon_degInt = lon_degInt;
}
void setPitch(float pitch) {
_pitch = pitch;
}
void setPitchRate(float pitchRate) {
_pitchRate = pitchRate;
}
void setRoll(float roll) {
_roll = roll;
}
void setRollRate(float rollRate) {
_rollRate = rollRate;
}
void setYaw(float yaw) {
_yaw = yaw;
}
void setYawRate(float yawRate) {
_yawRate = yawRate;
}
void setTimeStamp(int32_t timeStamp) {
_timeStamp = timeStamp;
}
int32_t getTimeStamp() const {
return _timeStamp;
}
void setWindDirection(float windDirection) {
_windDirection = windDirection;
}
void setWindSpeed(float windSpeed) {
_windSpeed = windSpeed;
}
protected:
AP_Board * _board;
private:
int32_t _timeStamp; /// time stamp for navigation data, micros clock
float _roll; /// roll angle, radians
float _rollRate; /// roll rate, radians/s
float _pitch; /// pitch angle, radians
float _pitchRate; /// pitch rate, radians/s
float _yaw; /// yaw angle, radians
float _yawRate; /// yaw rate, radians/s
// vertical
float _windSpeed; /// wind speed, m/s
float _windDirection; /// wind directioin, radians
float _vN; ///
float _vE;
float _vD; // m/s
float _xAccel;
float _yAccel;
float _zAccel;
int32_t _lat_degInt; // deg / 1e7
int32_t _lon_degInt; // deg / 1e7
int32_t _alt_intM; // meters / 1e3
};
} // namespace apo
#endif // AP_Navigator_H
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