ardupilot/Arducopter/Navigation.pde

/*
 ArduCopter v1.3 - August 2010
 www.ArduCopter.com
 Copyright (c) 2010.  All rights reserved.
 An Open Source Arduino based multicopter.
 
 This program 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 program 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/>.
*/

/* ************************************************************ */
/* GPS based Position control */
void Position_control(long lat_dest, long lon_dest)
{
  long Lon_diff;
  long Lat_diff;
  float gps_err_roll;
  float gps_err_pitch;

  Lon_diff = lon_dest - GPS.Longitude;
  Lat_diff = lat_dest - GPS.Lattitude;

  // ROLL
  gps_err_roll_old = gps_err_roll;
  //Optimization : cos(yaw) = DCM_Matrix[0][0] ;  sin(yaw) = DCM_Matrix[1][0] 
  gps_err_roll = (float)Lon_diff*GEOG_CORRECTION_FACTOR*DCM_Matrix[0][0] - (float)Lat_diff*DCM_Matrix[1][0];

  gps_roll_D = (gps_err_roll-gps_err_roll_old)/GPS_Dt;

  gps_roll_I += gps_err_roll*GPS_Dt;
  gps_roll_I = constrain(gps_roll_I,-800,800);

  command_gps_roll = KP_GPS_ROLL*gps_err_roll + KD_GPS_ROLL*gps_roll_D + KI_GPS_ROLL*gps_roll_I;
  command_gps_roll = constrain(command_gps_roll,-GPS_MAX_ANGLE,GPS_MAX_ANGLE); // Limit max command
  
  // PITCH
  gps_err_pitch_old = gps_err_pitch;
  gps_err_pitch = -(float)Lat_diff*DCM_Matrix[0][0]- (float)Lon_diff*GEOG_CORRECTION_FACTOR*DCM_Matrix[1][0];

  gps_pitch_D = (gps_err_pitch-gps_err_pitch_old)/GPS_Dt;

  gps_pitch_I += gps_err_pitch*GPS_Dt;
  gps_pitch_I = constrain(gps_pitch_I,-800,800);

  command_gps_pitch = KP_GPS_PITCH*gps_err_pitch + KD_GPS_PITCH*gps_pitch_D + KI_GPS_PITCH*gps_pitch_I;
  command_gps_pitch = constrain(command_gps_pitch,-GPS_MAX_ANGLE,GPS_MAX_ANGLE); // Limit max command
}

/* ************************************************************ */
/* Altitude control... (based on sonar)  // NOT TESTED!!*/
void Altitude_control(int target_sonar_altitude)
{
  err_altitude_old = err_altitude;
  err_altitude = target_sonar_altitude - Sonar_value;  
  altitude_D = (float)(err_altitude - err_altitude_old) / G_Dt;
  altitude_I += (float)err_altitude * G_Dt;
  altitude_I = constrain(altitude_I, -100, 100);
  command_altitude = Initial_Throttle + KP_ALTITUDE * err_altitude + KD_ALTITUDE * altitude_D + KI_ALTITUDE * altitude_I;
}