ardupilot/libraries/AP_Compass/Compass.cpp
Adam M Rivera c390db5d92 AP_Declination: Added method set_initial_location
This will set the declination based on lat/lon if the user has
not yet saved one to the EEPROM, OR if they have specified via the
config parameter that they want it to overwrite the declination every
3D fix.

Signed-off-by: Andrew Tridgell <tridge@samba.org>
2012-03-11 20:59:47 +11:00

233 lines
6.3 KiB
C++

/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
#include "Compass.h"
const AP_Param::GroupInfo Compass::var_info[] PROGMEM = {
// index 0 was used for the old orientation matrix
AP_GROUPINFO("OFS", 1, Compass, _offset),
AP_GROUPINFO("DEC", 2, Compass, _declination),
AP_GROUPINFO("LEARN", 3, Compass, _learn), // true if learning calibration
AP_GROUPINFO("USE", 4, Compass, _use_for_yaw), // true if used for DCM yaw
AP_GROUPEND
};
// Default constructor.
// Note that the Vector/Matrix constructors already implicitly zero
// their values.
//
Compass::Compass(void) :
product_id(AP_COMPASS_TYPE_UNKNOWN),
_declination (0.0),
_learn(1),
_use_for_yaw(1),
_null_enable(false),
_null_init_done(false),
_orientation(ROTATION_NONE)
{
}
// Default init method, just returns success.
//
bool
Compass::init()
{
return true;
}
void
Compass::set_orientation(enum Rotation rotation)
{
_orientation = rotation;
}
void
Compass::set_offsets(const Vector3f &offsets)
{
_offset.set(offsets);
}
void
Compass::save_offsets()
{
_offset.save();
}
Vector3f &
Compass::get_offsets()
{
return _offset;
}
bool
Compass::set_initial_location(long latitude, long longitude, bool force)
{
// If the user has choosen to use auto-declination regardless of the planner value
// OR
// If the declination failed to load from the EEPROM (ie. not set by user)
if(force || !_declination.load())
{
// Set the declination based on the lat/lng from GPS
_declination.set(radians(AP_Declination::get_declination((float)latitude / 10000000, (float)longitude / 10000000)));
// Reset null offsets
null_offsets_disable();
null_offsets_enable();
return true;
}
return false;
}
void
Compass::set_declination(float radians)
{
_declination.set_and_save(radians);
}
float
Compass::get_declination()
{
return _declination.get();
}
void
Compass::calculate(float roll, float pitch)
{
// Note - This function implementation is deprecated
// The alternate implementation of this function using the dcm matrix is preferred
float headX;
float headY;
float cos_roll;
float sin_roll;
float cos_pitch;
float sin_pitch;
cos_roll = cos(roll);
sin_roll = sin(roll);
cos_pitch = cos(pitch);
sin_pitch = sin(pitch);
// Tilt compensated magnetic field X component:
headX = mag_x*cos_pitch + mag_y*sin_roll*sin_pitch + mag_z*cos_roll*sin_pitch;
// Tilt compensated magnetic field Y component:
headY = mag_y*cos_roll - mag_z*sin_roll;
// magnetic heading
heading = atan2(-headY,headX);
// Declination correction (if supplied)
if( fabs(_declination) > 0.0 )
{
heading = heading + _declination;
if (heading > M_PI) // Angle normalization (-180 deg, 180 deg)
heading -= (2.0 * M_PI);
else if (heading < -M_PI)
heading += (2.0 * M_PI);
}
// Optimization for external DCM use. Calculate normalized components
heading_x = cos(heading);
heading_y = sin(heading);
}
void
Compass::calculate(const Matrix3f &dcm_matrix)
{
float headX;
float headY;
float cos_pitch = safe_sqrt(1-(dcm_matrix.c.x*dcm_matrix.c.x));
// sin(pitch) = - dcm_matrix(3,1)
// cos(pitch)*sin(roll) = - dcm_matrix(3,2)
// cos(pitch)*cos(roll) = - dcm_matrix(3,3)
if (cos_pitch == 0.0) {
// we are pointing straight up or down so don't update our
// heading using the compass. Wait for the next iteration when
// we hopefully will have valid values again.
return;
}
// Tilt compensated magnetic field X component:
headX = mag_x*cos_pitch - mag_y*dcm_matrix.c.y*dcm_matrix.c.x/cos_pitch - mag_z*dcm_matrix.c.z*dcm_matrix.c.x/cos_pitch;
// Tilt compensated magnetic field Y component:
headY = mag_y*dcm_matrix.c.z/cos_pitch - mag_z*dcm_matrix.c.y/cos_pitch;
// magnetic heading
// 6/4/11 - added constrain to keep bad values from ruining DCM Yaw - Jason S.
heading = constrain(atan2(-headY,headX), -3.15, 3.15);
// Declination correction (if supplied)
if( fabs(_declination) > 0.0 )
{
heading = heading + _declination;
if (heading > M_PI) // Angle normalization (-180 deg, 180 deg)
heading -= (2.0 * M_PI);
else if (heading < -M_PI)
heading += (2.0 * M_PI);
}
// Optimization for external DCM use. Calculate normalized components
heading_x = cos(heading);
heading_y = sin(heading);
#if 0
if (isnan(heading_x) || isnan(heading_y)) {
Serial.printf("COMPASS: c.x %f c.y %f c.z %f cos_pitch %f mag_x %d mag_y %d mag_z %d headX %f headY %f heading %f heading_x %f heading_y %f\n",
dcm_matrix.c.x,
dcm_matrix.c.y,
dcm_matrix.c.x,
cos_pitch,
(int)mag_x, (int)mag_y, (int)mag_z,
headX, headY,
heading,
heading_x, heading_y);
}
#endif
}
void
Compass::null_offsets(const Matrix3f &dcm_matrix)
{
if (_null_enable == false || _learn == 0) {
// auto-calibration is disabled
return;
}
// Update our estimate of the offsets in the magnetometer
Vector3f calc;
Matrix3f dcm_new_from_last;
float weight;
Vector3f mag_body_new = Vector3f(mag_x,mag_y,mag_z);
if(_null_init_done) {
dcm_new_from_last = dcm_matrix.transposed() * _last_dcm_matrix; // Note 11/20/2010: transpose() is not working, transposed() is.
weight = 3.0 - fabs(dcm_new_from_last.a.x) - fabs(dcm_new_from_last.b.y) - fabs(dcm_new_from_last.c.z);
if (weight > .001) {
calc = mag_body_new + _mag_body_last; // Eq 11 from Bill P's paper
calc -= dcm_new_from_last * _mag_body_last;
calc -= dcm_new_from_last.transposed() * mag_body_new;
if(weight > 0.5) weight = 0.5;
calc = calc * (weight);
_offset.set(_offset.get() - calc);
}
} else {
_null_init_done = true;
}
_mag_body_last = mag_body_new - calc;
_last_dcm_matrix = dcm_matrix;
}
void
Compass::null_offsets_enable(void)
{
_null_init_done = false;
_null_enable = true;
}
void
Compass::null_offsets_disable(void)
{
_null_init_done = false;
_null_enable = false;
}