mirror of https://github.com/ArduPilot/ardupilot
298 lines
6.5 KiB
C++
298 lines
6.5 KiB
C++
/*
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* AP_Navigator.h
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* Copyright (C) James Goppert 2010 <james.goppert@gmail.com>
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*
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* This file is free software: you can redistribute it and/or modify it
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* under the terms of the GNU General Public License as published by the
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* Free Software Foundation, either version 3 of the License, or
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* (at your option) any later version.
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*
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* This file is distributed in the hope that it will be useful, but
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* WITHOUT ANY WARRANTY; without even the implied warranty of
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* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.
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* See the GNU General Public License for more details.
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*
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* You should have received a copy of the GNU General Public License along
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* with this program. If not, see <http://www.gnu.org/licenses/>.
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*/
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#ifndef AP_Navigator_H
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#define AP_Navigator_H
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#include "constants.h"
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#include <inttypes.h>
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namespace apo {
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class AP_Board;
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/// Navigator class
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class AP_Navigator {
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public:
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AP_Navigator(AP_Board * board);
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// note, override these with derived navigator functionality
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virtual void calibrate() {};
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virtual void updateFast(float dt) {};
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virtual void updateSlow(float dt) {};
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// accessors
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float getPD() const;
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float getPE() const;
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float getPN() const;
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void setPD(float _pD);
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void setPE(float _pE);
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void setPN(float _pN);
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float getAirSpeed() const {
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// neglects vertical wind
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float vWN = getVN() + getWindSpeed()*cos(getWindDirection());
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float vWE = getVE() + getWindSpeed()*sin(getWindDirection());
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return sqrt(vWN*vWN+vWE+vWE+getVD()*getVD());
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}
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float getGroundSpeed() const {
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return sqrt(getVN()*getVN()+getVE()*getVE());
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}
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float getWindSpeed() const {
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return _windSpeed;
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}
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int32_t getAlt_intM() const {
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return _alt_intM;
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}
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float getAlt() const {
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return _alt_intM / scale_m;
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}
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void setAlt(float _alt) {
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this->_alt_intM = _alt * scale_m;
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}
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float getLat() const {
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//Serial.print("getLatfirst");
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//Serial.println(_lat_degInt * degInt2Rad);
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return _lat_degInt * degInt2Rad;
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}
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void setLat(float _lat) {
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//Serial.print("setLatfirst");
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//Serial.println(_lat * rad2DegInt);
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setLat_degInt(_lat*rad2DegInt);
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}
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float getLon() const {
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return _lon_degInt * degInt2Rad;
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}
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void setLon(float _lon) {
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this->_lon_degInt = _lon * rad2DegInt;
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}
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float getVN() const {
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return _vN;
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}
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float getVE() const {
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return _vE;
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}
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float getVD() const {
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return _vD;
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}
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int32_t getLat_degInt() const {
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//Serial.print("getLat_degInt");
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//Serial.println(_lat_degInt);
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return _lat_degInt;
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}
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int32_t getLon_degInt() const {
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return _lon_degInt;
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}
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float getPitch() const {
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return _pitch;
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}
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float getPitchRate() const {
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return _pitchRate;
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}
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float getRoll() const {
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return _roll;
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}
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float getRollRate() const {
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return _rollRate;
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}
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float getYaw() const {
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return _yaw;
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}
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float getYawRate() const {
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return _yawRate;
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}
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float getWindDirection() const {
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return _windDirection;
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}
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float getCourseOverGround() const {
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return atan2(getVE(),getVN());
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}
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float getRelativeCourseOverGround() const {
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float y = getCourseOverGround() - getYaw();
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if (y > 180 * deg2Rad)
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y -= 360 * deg2Rad;
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if (y < -180 * deg2Rad)
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y += 360 * deg2Rad;
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return y;
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}
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float getSpeedOverGround() const {
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return sqrt(getVN()*getVN()+getVE()*getVE());
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}
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float getXAccel() const {
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return _xAccel;
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}
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float getYAccel() const {
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return _yAccel;
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}
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float getZAccel() const {
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return _zAccel;
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}
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void setAirSpeed(float airSpeed) {
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// assumes wind constant and rescale navigation speed
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float vScale = (1 + airSpeed/getAirSpeed());
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float vNorm = sqrt(getVN()*getVN()+getVE()*getVE()+getVD()*getVD());
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_vN *= vScale/vNorm;
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_vE *= vScale/vNorm;
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_vD *= vScale/vNorm;
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}
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void setAlt_intM(int32_t alt_intM) {
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_alt_intM = alt_intM;
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}
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void setVN(float vN) {
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_vN = vN;
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}
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void setVE(float vE) {
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_vE = vE;
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}
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void setVD(float vD) {
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_vD = vD;
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}
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void setXAccel(float xAccel) {
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_xAccel = xAccel;
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}
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void setYAccel(float yAccel) {
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_yAccel = yAccel;
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}
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void setZAccel(float zAccel) {
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_zAccel = zAccel;
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}
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void setGroundSpeed(float groundSpeed) {
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float cog = getCourseOverGround();
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_vN = cos(cog)*groundSpeed;
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_vE = sin(cog)*groundSpeed;
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}
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void setLat_degInt(int32_t lat_degInt) {
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_lat_degInt = lat_degInt;
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//Serial.print("setLat_degInt");
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//Serial.println(_lat_degInt);
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}
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void setLon_degInt(int32_t lon_degInt) {
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_lon_degInt = lon_degInt;
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}
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void setPitch(float pitch) {
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_pitch = pitch;
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}
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void setPitchRate(float pitchRate) {
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_pitchRate = pitchRate;
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}
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void setRoll(float roll) {
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_roll = roll;
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}
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void setRollRate(float rollRate) {
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_rollRate = rollRate;
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}
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void setYaw(float yaw) {
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_yaw = yaw;
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}
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void setYawRate(float yawRate) {
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_yawRate = yawRate;
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}
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void setTimeStamp(int32_t timeStamp) {
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_timeStamp = timeStamp;
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}
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int32_t getTimeStamp() const {
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return _timeStamp;
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}
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void setWindDirection(float windDirection) {
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_windDirection = windDirection;
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}
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void setWindSpeed(float windSpeed) {
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_windSpeed = windSpeed;
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}
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protected:
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AP_Board * _board;
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private:
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int32_t _timeStamp; /// time stamp for navigation data, micros clock
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float _roll; /// roll angle, radians
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float _rollRate; /// roll rate, radians/s
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float _pitch; /// pitch angle, radians
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float _pitchRate; /// pitch rate, radians/s
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float _yaw; /// yaw angle, radians
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float _yawRate; /// yaw rate, radians/s
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// vertical
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float _windSpeed; /// wind speed, m/s
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float _windDirection; /// wind directioin, radians
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float _vN; ///
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float _vE;
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float _vD; // m/s
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float _xAccel;
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float _yAccel;
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float _zAccel;
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int32_t _lat_degInt; // deg / 1e7
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int32_t _lon_degInt; // deg / 1e7
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int32_t _alt_intM; // meters / 1e3
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};
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} // namespace apo
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#endif // AP_Navigator_H
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// vim:ts=4:sw=4:expandtab
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