mirror of https://github.com/ArduPilot/ardupilot
fixed inverted cos error
git-svn-id: https://arducopter.googlecode.com/svn/trunk@1597 f9c3cf11-9bcb-44bc-f272-b75c42450872
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@ -41,9 +41,12 @@ void navigate()
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update_navigation();
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update_navigation();
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}
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}
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#define DIST_ERROR_MAX 3000
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#define DIST_ERROR_MAX 1800
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void calc_nav()
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void calc_nav()
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{
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{
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Vector2f yawvector;
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long long_error, lat_error;
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/*
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/*
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Becuase we are using lat and lon to do our distance errors here's a quick chart:
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Becuase we are using lat and lon to do our distance errors here's a quick chart:
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100 = 1m
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100 = 1m
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@ -53,23 +56,31 @@ void calc_nav()
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pitch_max = 22° (2200)
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pitch_max = 22° (2200)
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*/
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*/
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Vector2f yawvector;
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Matrix3f temp = dcm.get_dcm_matrix();
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Matrix3f temp = dcm.get_dcm_matrix();
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yawvector.x = temp.a.x; // sin
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yawvector.x = temp.a.x;
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yawvector.y = temp.b.x; // cos
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yawvector.y = temp.b.x;
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yawvector.normalize();
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yawvector.normalize();
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yawvector.y = -yawvector.y;
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//cos =
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long_error = (float)(next_WP.lng - current_loc.lng) * scaleLongDown;
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lat_error = next_WP.lat - current_loc.lat;
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long_error = constrain(long_error, -DIST_ERROR_MAX, DIST_ERROR_MAX); // +- 20m max error
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lat_error = constrain(lat_error, -DIST_ERROR_MAX, DIST_ERROR_MAX); // +- 20m max error
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// ROLL
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// ROLL
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nav_lon = pid_nav_lon.get_pid((long)((float)(next_WP.lng - GPS.longitude) * scaleLongDown), dTnav, 1.0);
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nav_lon = long_error * pid_nav_lon.kP();
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nav_lon = constrain(nav_lon, -DIST_ERROR_MAX, DIST_ERROR_MAX); // Limit max command
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//nav_lon = pid_nav_lon.get_pid(long_error, dTnav2, 1.0);
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//nav_lon = constrain(nav_lon, -DIST_ERROR_MAX, DIST_ERROR_MAX); // Limit max command
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// PITCH
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// PITCH
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nav_lat = pid_nav_lat.get_pid(next_WP.lat - GPS.latitude, dTnav, 1.0);
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//nav_lat = pid_nav_lat.get_pid(lat_error, dTnav2, 1.0);
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nav_lat = constrain(nav_lat, -DIST_ERROR_MAX, DIST_ERROR_MAX); // Limit max command
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nav_lat = lat_error * pid_nav_lat.kP();
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//nav_lat = constrain(nav_lat, -DIST_ERROR_MAX, DIST_ERROR_MAX); // Limit max command
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// rotate the vector
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// rotate the vector
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nav_roll = (float)nav_lon * yawvector.x + (float)nav_lat * yawvector.y;
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nav_roll = (float)nav_lon * yawvector.x - (float)nav_lat * yawvector.y;
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nav_pitch = (float)nav_lat * yawvector.x + (float)nav_lon * yawvector.y;
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nav_pitch = (float)nav_lat * yawvector.x + (float)nav_lon * yawvector.y;
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//Serial.printf("vx %4.4f,vy %4.4f ", yawvector.x, yawvector.y);
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//Serial.printf("vx %4.4f,vy %4.4f ", yawvector.x, yawvector.y);
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