Loiter should work now.

git-svn-id: https://arducopter.googlecode.com/svn/trunk@1921 f9c3cf11-9bcb-44bc-f272-b75c42450872
This commit is contained in:
jasonshort 2011-04-26 05:15:25 +00:00
parent 7e843ee679
commit 93a7a76c9b
4 changed files with 57 additions and 29 deletions

View File

@ -257,6 +257,7 @@ int climb_rate; // m/s * 100 - For future implementation of controlled a
float nav_gain_scaler = 1; // Gain scaling for headwind/tailwind TODO: why does this variable need to be initialized to 1?
int last_ground_speed; // used to dampen navigation
byte wp_control; // used to control - navgation or loiter
byte command_must_index; // current command memory location
byte command_may_index; // current command memory location
@ -327,9 +328,6 @@ byte yaw_tracking = TRACK_NONE; // no tracking, point at next wp, or at a tar
// Loiter management
// -----------------
long saved_target_bearing; // deg * 100
//int loiter_total; // deg : how many times to loiter * 360
//int loiter_delta; // deg : how far we just turned
//int loiter_sum; // deg : how far we have turned around a waypoint
long loiter_time; // millis : when we started LOITER mode
long loiter_time_max; // millis : how long to stay in LOITER mode
@ -591,21 +589,6 @@ void medium_loop()
// --------------------------------------------
update_navigation();
}
// we call these regardless of GPS because of the rapid nature of the yaw sensor
// -----------------------------------------------------------------------------
//if(wp_distance < 800){ // 8 meters
//if(g.rc_6.control_in > 500){ // 8 meters
//calc_loiter_nav();
// calc_waypoint_nav();
//}else{
// calc_waypoint_nav();
//}
invalid_nav = true;
// replace with invalidater byte
//calc_waypoint_nav();
break;
// command processing
@ -946,7 +929,6 @@ void update_current_flight_mode(void)
}
break;
//case LOITER:
case STABILIZE:
// clear any AP naviagtion values
nav_pitch = 0;
@ -1107,11 +1089,17 @@ void update_navigation()
if(control_mode == AUTO || control_mode == GCS_AUTO){
verify_commands();
// calc a rate dampened pitch to the target
calc_rate_nav();
if(wp_control == LOITER_MODE){
// calc a pitch to the target
calc_loiter_nav();
// rotate that pitch to the copter frame of reference
calc_nav_output();
} else {
// calc a rate dampened pitch to the target
calc_rate_nav();
// rotate that pitch to the copter frame of reference
calc_nav_output();
}
//limit our copter pitch - this will change if we go to a fully rate limited approach.
limit_nav_pitch_roll(g.pitch_max.get());
@ -1122,8 +1110,22 @@ void update_navigation()
}
}else{
switch(control_mode){
case LOITER:
// calc a pitch to the target
calc_loiter_nav();
// limit tilt
limit_nav_pitch_roll(g.pitch_max.get());
break;
case RTL:
// calc a pitch to the target
calc_loiter_nav();
// limit tilt
limit_nav_pitch_roll(g.pitch_max.get());
update_crosstrack();
break;
}
@ -1169,6 +1171,8 @@ void update_alt()
// read barometer
baro_alt = read_barometer();
// XXX temp removed fr debugging
//filter out bad sonar reads
//int temp = sonar.read();
@ -1182,12 +1186,15 @@ void update_alt()
update_sonar_light(sonar_alt > 100);
// decide if we're using sonar
if (baro_alt < 1200){
if ((baro_alt < 1200) || sonar_alt < 300){
// correct alt for angle of the sonar
sonar_alt = (float)sonar_alt * (cos_pitch_x * cos_roll_x);
float temp = cos_pitch_x * cos_roll_x;
temp = max(temp, 0.707);
if(sonar_alt < 500){
sonar_alt = (float)sonar_alt * temp;
if(sonar_alt < 400){
altitude_sensor = SONAR;
}
}

View File

@ -193,11 +193,13 @@ bool verify_may()
}
/********************************************************************************/
// Nav (Must) commands
//
/********************************************************************************/
void do_RTL(void)
{
// we need to change this.
wp_control = LOITER_MODE;
control_mode = LOITER;
Location temp = home;
temp.alt = read_alt_to_hold();
@ -216,8 +218,14 @@ void do_RTL(void)
// Log_Write_Mode(control_mode);
}
/********************************************************************************/
// Nav (Must) commands
/********************************************************************************/
void do_takeoff()
{
wp_control = LOITER_MODE;
Location temp = current_loc;
// next_command.alt is a relative altitude!!!
@ -233,6 +241,8 @@ void do_takeoff()
void do_nav_wp()
{
wp_control = WP_MODE;
// next_command.alt is a relative altitude!!!
next_command.alt += home.alt;
@ -256,6 +266,8 @@ void do_nav_wp()
void do_land()
{
wp_control = LOITER_MODE;
Serial.println("dlnd ");
// not really used right now, might be good for debugging
@ -276,6 +288,8 @@ void do_land()
void do_loiter_unlimited()
{
wp_control = LOITER_MODE;
//Serial.println("dloi ");
if(next_command.lat == 0)
set_next_WP(&current_loc);
@ -286,6 +300,8 @@ void do_loiter_unlimited()
void do_loiter_turns()
{
/*
wp_control = LOITER_MODE;
if(next_command.lat == 0)
set_next_WP(&current_loc);
else
@ -298,6 +314,7 @@ void do_loiter_turns()
void do_loiter_time()
{
/*
wp_control = LOITER_MODE;
if(next_command.lat == 0)
set_next_WP(&current_loc);
else
@ -393,6 +410,9 @@ bool verify_nav_wp()
if(wp_verify_byte & NAV_LOCATION){
// we have reached our goal
// loiter at the WP
wp_control = LOITER_MODE;
if ((millis() - loiter_time) > loiter_time_max) {
wp_verify_byte |= NAV_DELAY;
//gcs.send_text_P(SEVERITY_LOW,PSTR("verify_must: LOITER time complete"));

View File

@ -129,6 +129,9 @@
#define TRACK_NEXT_WP 2
#define TRACK_TARGET_WP 4
#define LOITER_MODE 1
#define WP_MODE 2
// Waypoint options
#define WP_OPTION_ALT_RELATIVE 1
#define WP_OPTION_ALT_CHANGE 2

View File

@ -224,8 +224,6 @@ void update_crosstrack(void)
crosstrack_error = sin(radians((target_bearing - crosstrack_bearing) / 100)) * wp_distance; // Meters we are off track line
nav_bearing += constrain(crosstrack_error * g.crosstrack_gain, -g.crosstrack_entry_angle.get(), g.crosstrack_entry_angle.get());
nav_bearing = wrap_360(nav_bearing);
}else{
reset_crosstrack();
}
}