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uncrustify ArduPlane/navigation.pde

mission-4.1.18
uncrustify 13 years ago committed by Pat Hickey
parent
commit
909e39d667
  1. 204
      ArduPlane/navigation.pde

204
ArduPlane/navigation.pde

@ -5,48 +5,48 @@ @@ -5,48 +5,48 @@
//****************************************************************
static void navigate()
{
// do not navigate with corrupt data
// ---------------------------------
if (!have_position) {
return;
}
if(next_WP.lat == 0){
return;
}
// waypoint distance from plane
// ----------------------------
wp_distance = get_distance(&current_loc, &next_WP);
if (wp_distance < 0) {
gcs_send_text_P(SEVERITY_HIGH,PSTR("WP error - distance < 0"));
//Serial.println(wp_distance,DEC);
return;
}
// target_bearing is where we should be heading
// --------------------------------------------
target_bearing_cd = get_bearing_cd(&current_loc, &next_WP);
// nav_bearing will includes xtrac correction
// ------------------------------------------
nav_bearing_cd = target_bearing_cd;
// check if we have missed the WP
loiter_delta = (target_bearing_cd - old_target_bearing_cd)/100;
// reset the old value
old_target_bearing_cd = target_bearing_cd;
// wrap values
if (loiter_delta > 180) loiter_delta -= 360;
if (loiter_delta < -180) loiter_delta += 360;
loiter_sum += abs(loiter_delta);
// control mode specific updates to nav_bearing
// --------------------------------------------
update_navigation();
// do not navigate with corrupt data
// ---------------------------------
if (!have_position) {
return;
}
if(next_WP.lat == 0) {
return;
}
// waypoint distance from plane
// ----------------------------
wp_distance = get_distance(&current_loc, &next_WP);
if (wp_distance < 0) {
gcs_send_text_P(SEVERITY_HIGH,PSTR("WP error - distance < 0"));
//Serial.println(wp_distance,DEC);
return;
}
// target_bearing is where we should be heading
// --------------------------------------------
target_bearing_cd = get_bearing_cd(&current_loc, &next_WP);
// nav_bearing will includes xtrac correction
// ------------------------------------------
nav_bearing_cd = target_bearing_cd;
// check if we have missed the WP
loiter_delta = (target_bearing_cd - old_target_bearing_cd)/100;
// reset the old value
old_target_bearing_cd = target_bearing_cd;
// wrap values
if (loiter_delta > 180) loiter_delta -= 360;
if (loiter_delta < -180) loiter_delta += 360;
loiter_sum += abs(loiter_delta);
// control mode specific updates to nav_bearing
// --------------------------------------------
update_navigation();
}
@ -54,9 +54,9 @@ static void navigate() @@ -54,9 +54,9 @@ static void navigate()
// Disabled for now
void calc_distance_error()
{
distance_estimate += (float)g_gps->ground_speed * .0002 * cos(radians(bearing_error_cd * .01));
distance_estimate -= DST_EST_GAIN * (float)(distance_estimate - GPS_wp_distance);
wp_distance = max(distance_estimate,10);
distance_estimate += (float)g_gps->ground_speed * .0002 * cos(radians(bearing_error_cd * .01));
distance_estimate -= DST_EST_GAIN * (float)(distance_estimate - GPS_wp_distance);
wp_distance = max(distance_estimate,10);
}
#endif
@ -70,9 +70,9 @@ static void calc_airspeed_errors() @@ -70,9 +70,9 @@ static void calc_airspeed_errors()
// FBW_B airspeed target
if (control_mode == FLY_BY_WIRE_B) {
target_airspeed_cm = ((int)(g.flybywire_airspeed_max -
g.flybywire_airspeed_min) *
g.channel_throttle.servo_out) +
((int)g.flybywire_airspeed_min * 100);
g.flybywire_airspeed_min) *
g.channel_throttle.servo_out) +
((int)g.flybywire_airspeed_min * 100);
}
// Set target to current airspeed + ground speed undershoot,
@ -106,85 +106,85 @@ static void calc_gndspeed_undershoot() @@ -106,85 +106,85 @@ static void calc_gndspeed_undershoot()
static void calc_bearing_error()
{
bearing_error_cd = nav_bearing_cd - ahrs.yaw_sensor;
bearing_error_cd = wrap_180_cd(bearing_error_cd);
bearing_error_cd = wrap_180_cd(bearing_error_cd);
}
static void calc_altitude_error()
{
if(control_mode == AUTO && offset_altitude_cm != 0) {
// limit climb rates
target_altitude_cm = next_WP.alt - ((float)((wp_distance -30) * offset_altitude_cm) / (float)(wp_totalDistance - 30));
// stay within a certain range
if(prev_WP.alt > next_WP.alt){
target_altitude_cm = constrain(target_altitude_cm, next_WP.alt, prev_WP.alt);
}else{
target_altitude_cm = constrain(target_altitude_cm, prev_WP.alt, next_WP.alt);
}
} else if (non_nav_command_ID != MAV_CMD_CONDITION_CHANGE_ALT) {
target_altitude_cm = next_WP.alt;
}
altitude_error_cm = target_altitude_cm - current_loc.alt;
if(control_mode == AUTO && offset_altitude_cm != 0) {
// limit climb rates
target_altitude_cm = next_WP.alt - ((float)((wp_distance -30) * offset_altitude_cm) / (float)(wp_totalDistance - 30));
// stay within a certain range
if(prev_WP.alt > next_WP.alt) {
target_altitude_cm = constrain(target_altitude_cm, next_WP.alt, prev_WP.alt);
}else{
target_altitude_cm = constrain(target_altitude_cm, prev_WP.alt, next_WP.alt);
}
} else if (non_nav_command_ID != MAV_CMD_CONDITION_CHANGE_ALT) {
target_altitude_cm = next_WP.alt;
}
altitude_error_cm = target_altitude_cm - current_loc.alt;
}
static int32_t wrap_360_cd(int32_t error)
{
if (error > 36000) error -= 36000;
if (error < 0) error += 36000;
return error;
if (error > 36000) error -= 36000;
if (error < 0) error += 36000;
return error;
}
static int32_t wrap_180_cd(int32_t error)
{
if (error > 18000) error -= 36000;
if (error < -18000) error += 36000;
return error;
if (error > 18000) error -= 36000;
if (error < -18000) error += 36000;
return error;
}
static void update_loiter()
{
float power;
if(wp_distance <= g.loiter_radius){
power = float(wp_distance) / float(g.loiter_radius);
power = constrain(power, 0.5, 1);
nav_bearing_cd += 9000.0 * (2.0 + power);
} else if(wp_distance < (g.loiter_radius + LOITER_RANGE)){
power = -((float)(wp_distance - g.loiter_radius - LOITER_RANGE) / LOITER_RANGE);
power = constrain(power, 0.5, 1); //power = constrain(power, 0, 1);
nav_bearing_cd -= power * 9000;
} else{
update_crosstrack();
loiter_time_ms = millis(); // keep start time for loiter updating till we get within LOITER_RANGE of orbit
}
float power;
if(wp_distance <= g.loiter_radius) {
power = float(wp_distance) / float(g.loiter_radius);
power = constrain(power, 0.5, 1);
nav_bearing_cd += 9000.0 * (2.0 + power);
} else if(wp_distance < (g.loiter_radius + LOITER_RANGE)) {
power = -((float)(wp_distance - g.loiter_radius - LOITER_RANGE) / LOITER_RANGE);
power = constrain(power, 0.5, 1); //power = constrain(power, 0, 1);
nav_bearing_cd -= power * 9000;
} else{
update_crosstrack();
loiter_time_ms = millis(); // keep start time for loiter updating till we get within LOITER_RANGE of orbit
}
/*
if (wp_distance < g.loiter_radius){
nav_bearing += 9000;
}else{
nav_bearing -= 100 * M_PI / 180 * asin(g.loiter_radius / wp_distance);
}
update_crosstrack();
*/
nav_bearing_cd = wrap_360_cd(nav_bearing_cd);
* if (wp_distance < g.loiter_radius){
* nav_bearing += 9000;
* }else{
* nav_bearing -= 100 * M_PI / 180 * asin(g.loiter_radius / wp_distance);
* }
*
* update_crosstrack();
*/
nav_bearing_cd = wrap_360_cd(nav_bearing_cd);
}
static void update_crosstrack(void)
{
// Crosstrack Error
// ----------------
// Crosstrack Error
// ----------------
// If we are too far off or too close we don't do track following
if (abs(wrap_180_cd(target_bearing_cd - crosstrack_bearing_cd)) < 4500) {
crosstrack_error = sin(radians((target_bearing_cd - crosstrack_bearing_cd) * 0.01)) * wp_distance; // Meters we are off track line
nav_bearing_cd += constrain(crosstrack_error * g.crosstrack_gain, -g.crosstrack_entry_angle.get(), g.crosstrack_entry_angle.get());
nav_bearing_cd = wrap_360_cd(nav_bearing_cd);
}
if (abs(wrap_180_cd(target_bearing_cd - crosstrack_bearing_cd)) < 4500) {
crosstrack_error = sin(radians((target_bearing_cd - crosstrack_bearing_cd) * 0.01)) * wp_distance; // Meters we are off track line
nav_bearing_cd += constrain(crosstrack_error * g.crosstrack_gain, -g.crosstrack_entry_angle.get(), g.crosstrack_entry_angle.get());
nav_bearing_cd = wrap_360_cd(nav_bearing_cd);
}
}
static void reset_crosstrack()
{
crosstrack_bearing_cd = get_bearing_cd(&prev_WP, &next_WP); // Used for track following
crosstrack_bearing_cd = get_bearing_cd(&prev_WP, &next_WP); // Used for track following
}

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