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/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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/********************************************************************************/
// Command Event Handlers
/********************************************************************************/
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// process_nav_command - main switch statement to initiate the next nav command in the command_nav_queue
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static void process_nav_command()
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{
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switch(command_nav_queue.id) {
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case MAV_CMD_NAV_TAKEOFF: // 22
do_takeoff();
break;
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case MAV_CMD_NAV_WAYPOINT: // 16 Navigate to Waypoint
do_nav_wp();
break;
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case MAV_CMD_NAV_LAND: // 21 LAND to Waypoint
do_land();
break;
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case MAV_CMD_NAV_LOITER_UNLIM: // 17 Loiter indefinitely
do_loiter_unlimited();
break;
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case MAV_CMD_NAV_LOITER_TURNS: //18 Loiter N Times
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do_circle();
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break;
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case MAV_CMD_NAV_LOITER_TIME: // 19
do_loiter_time();
break;
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case MAV_CMD_NAV_RETURN_TO_LAUNCH: //20
do_RTL();
break;
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// point the copter and camera at a region of interest (ROI)
case MAV_CMD_NAV_ROI: // 80
do_nav_roi();
break;
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default:
break;
}
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}
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static void process_cond_command()
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{
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switch(command_cond_queue.id) {
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case MAV_CMD_CONDITION_DELAY: // 112
do_wait_delay();
break;
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case MAV_CMD_CONDITION_DISTANCE: // 114
do_within_distance();
break;
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case MAV_CMD_CONDITION_CHANGE_ALT: // 113
do_change_alt();
break;
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case MAV_CMD_CONDITION_YAW: // 115
do_yaw();
break;
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default:
break;
}
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}
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static void process_now_command()
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{
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switch(command_cond_queue.id) {
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case MAV_CMD_DO_JUMP: // 177
do_jump();
break;
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case MAV_CMD_DO_CHANGE_SPEED: // 178
do_change_speed();
break;
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case MAV_CMD_DO_SET_HOME: // 179
do_set_home();
break;
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case MAV_CMD_DO_SET_SERVO: // 183
do_set_servo();
break;
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case MAV_CMD_DO_SET_RELAY: // 181
do_set_relay();
break;
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case MAV_CMD_DO_REPEAT_SERVO: // 184
do_repeat_servo();
break;
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case MAV_CMD_DO_REPEAT_RELAY: // 182
do_repeat_relay();
break;
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#if CAMERA == ENABLED
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case MAV_CMD_DO_CONTROL_VIDEO: // Control on-board camera capturing. |Camera ID (-1 for all)| Transmission: 0: disabled, 1: enabled compressed, 2: enabled raw| Transmission mode: 0: video stream, >0: single images every n seconds (decimal)| Recording: 0: disabled, 1: enabled compressed, 2: enabled raw| Empty| Empty| Empty|
break;
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case MAV_CMD_DO_DIGICAM_CONFIGURE: // Mission command to configure an on-board camera controller system. |Modes: P, TV, AV, M, Etc| Shutter speed: Divisor number for one second| Aperture: F stop number| ISO number e.g. 80, 100, 200, Etc| Exposure type enumerator| Command Identity| Main engine cut-off time before camera trigger in seconds/10 (0 means no cut-off)|
break;
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case MAV_CMD_DO_DIGICAM_CONTROL: // Mission command to control an on-board camera controller system. |Session control e.g. show/hide lens| Zoom's absolute position| Zooming step value to offset zoom from the current position| Focus Locking, Unlocking or Re-locking| Shooting Command| Command Identity| Empty|
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do_take_picture();
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break;
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#endif
#if MOUNT == ENABLED
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case MAV_CMD_DO_MOUNT_CONFIGURE: // Mission command to configure a camera mount |Mount operation mode (see MAV_CONFIGURE_MOUNT_MODE enum)| stabilize roll? (1 = yes, 0 = no)| stabilize pitch? (1 = yes, 0 = no)| stabilize yaw? (1 = yes, 0 = no)| Empty| Empty| Empty|
camera_mount.configure_cmd();
break;
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case MAV_CMD_DO_MOUNT_CONTROL: // Mission command to control a camera mount |pitch(deg*100) or lat, depending on mount mode.| roll(deg*100) or lon depending on mount mode| yaw(deg*100) or alt (in cm) depending on mount mode| Empty| Empty| Empty| Empty|
camera_mount.control_cmd();
break;
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#endif
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default:
// do nothing with unrecognized MAVLink messages
break;
}
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}
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/********************************************************************************/
// Verify command Handlers
/********************************************************************************/
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// verify_must - switch statement to ensure the active navigation command is progressing
// returns true once the active navigation command completes successfully
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static bool verify_must()
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{
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switch(command_nav_queue.id) {
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case MAV_CMD_NAV_TAKEOFF:
return verify_takeoff();
break;
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case MAV_CMD_NAV_WAYPOINT:
return verify_nav_wp();
break;
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case MAV_CMD_NAV_LAND:
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return verify_land();
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break;
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case MAV_CMD_NAV_LOITER_UNLIM:
return verify_loiter_unlimited();
break;
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case MAV_CMD_NAV_LOITER_TURNS:
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return verify_circle();
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break;
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case MAV_CMD_NAV_LOITER_TIME:
return verify_loiter_time();
break;
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case MAV_CMD_NAV_RETURN_TO_LAUNCH:
return verify_RTL();
break;
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case MAV_CMD_NAV_ROI: // 80
return verify_nav_roi();
break;
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default:
//gcs_send_text_P(SEVERITY_HIGH,PSTR("<verify_must: default> No current Must commands"));
return false;
break;
}
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}
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// verify_may - switch statement to ensure the active conditional command is progressing
// returns true once the active conditional command completes successfully
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static bool verify_may()
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{
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switch(command_cond_queue.id) {
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case MAV_CMD_CONDITION_DELAY:
return verify_wait_delay();
break;
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case MAV_CMD_CONDITION_DISTANCE:
return verify_within_distance();
break;
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case MAV_CMD_CONDITION_CHANGE_ALT:
return verify_change_alt();
break;
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case MAV_CMD_CONDITION_YAW:
return verify_yaw();
break;
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default:
//gcs_send_text_P(SEVERITY_HIGH,PSTR("<verify_must: default> No current May commands"));
return false;
break;
}
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}
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/********************************************************************************/
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//
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/********************************************************************************/
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// do_RTL - start Return-to-Launch
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static void do_RTL(void)
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{
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// set rtl state
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rtl_state = RTL_STATE_INITIAL_CLIMB;
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// set roll, pitch and yaw modes
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set_roll_pitch_mode(RTL_RP);
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set_yaw_mode(YAW_HOLD); // first stage of RTL is the initial climb so just hold current yaw
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set_throttle_mode(RTL_THR);
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// set navigation mode
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set_nav_mode(NAV_LOITER);
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// override altitude to RTL altitude
set_new_altitude(get_RTL_alt());
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}
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/********************************************************************************/
// Nav (Must) commands
/********************************************************************************/
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// do_takeoff - initiate takeoff navigation command
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static void do_takeoff()
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{
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// set roll-pitch mode
set_roll_pitch_mode(AUTO_RP);
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// set yaw mode
set_yaw_mode(YAW_HOLD);
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// set throttle mode to AUTO although we should already be in this mode
set_throttle_mode(THROTTLE_AUTO);
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// set target altitude
set_new_altitude(command_nav_queue.alt);
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// set our nav mode to loiter
set_nav_mode(NAV_LOITER);
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// prevent flips
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// To-Do: check if this is still necessary
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reset_I_all();
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}
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// do_nav_wp - initiate move to next waypoint
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// note: caller should set yaw mode
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static void do_nav_wp()
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{
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// set roll-pitch mode
set_roll_pitch_mode(AUTO_RP);
// set throttle mode
set_throttle_mode(THROTTLE_AUTO);
set_new_altitude(command_nav_queue.alt);
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// set nav mode
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set_nav_mode(NAV_WP);
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// Set inav navigation target
wpinav_set_destination(command_nav_queue);
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// this is our bitmask to verify we have met all conditions to move on
wp_verify_byte = 0;
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// if not delay requirement, set the delay achieved bit of wp_verify_byte
if( command_nav_queue.p1 == 0 ) {
wp_verify_byte |= NAV_DELAY;
}else{
// this will be used to remember the time in millis after we reach or pass the WP.
loiter_time = 0;
// this is the delay, stored in seconds and expanded to millis
loiter_time_max = command_nav_queue.p1 * 1000;
}
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// reset control of yaw to default
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if( g.yaw_override_behaviour == YAW_OVERRIDE_BEHAVIOUR_AT_NEXT_WAYPOINT ) {
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set_yaw_mode(AUTO_YAW);
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}
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}
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// do_land - initiate landing procedure
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// caller should set roll_pitch_mode to ROLL_PITCH_AUTO (for no pilot input) or ROLL_PITCH_LOITER (for pilot input)
// caller should set yaw_mode
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static void do_land()
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{
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if( ap.home_is_set ) {
// switch to loiter if we have gps
set_roll_pitch_mode(ROLL_PITCH_LOITER);
}else{
// otherwise remain with stabilize roll and pitch
set_roll_pitch_mode(ROLL_PITCH_STABLE);
}
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// hold yaw while landing
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set_yaw_mode(YAW_HOLD);
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// set throttle mode to land
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set_throttle_mode(THROTTLE_LAND);
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// switch into loiter nav mode
set_nav_mode(NAV_LOITER);
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}
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// do_loiter_unlimited - start loitering with no end conditions
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// note: caller should set yaw_mode
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static void do_loiter_unlimited()
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{
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// set roll-pitch mode (no pilot input)
set_roll_pitch_mode(AUTO_RP);
// set throttle mode to AUTO which, if not already active, will default to hold at our current altitude
set_throttle_mode(THROTTLE_AUTO);
// set target altitude if provided
if( command_nav_queue.alt != 0 ) {
set_new_altitude(command_nav_queue.alt);
}
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// if no location specified loiter at current location
if(command_nav_queue.lat == 0 && command_nav_queue.lng == 0) {
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set_nav_mode(NAV_LOITER);
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}else{
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// location specified so fly to the target location
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set_nav_mode(NAV_WP);
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// Set inav navigation target
wpinav_set_destination(command_nav_queue);
}
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}
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// do_circle - initiate moving in a circle
static void do_circle()
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{
// set roll-pitch mode (no pilot input)
set_roll_pitch_mode(AUTO_RP);
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// set throttle mode to AUTO which, if not already active, will default to hold at our current altitude
set_throttle_mode(THROTTLE_AUTO);
// set target altitude if provided
if( command_nav_queue.alt != 0 ) {
set_new_altitude(command_nav_queue.alt);
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}
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// set nav mode to CIRCLE
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set_nav_mode(NAV_CIRCLE);
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// override default horizontal location target
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if( command_nav_queue.lat != 0 || command_nav_queue.lng != 0) {
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circle_set_center(pv_latlon_to_vector(command_nav_queue.lat, command_nav_queue.lng), ahrs.yaw);
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}
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// set yaw to point to center of circle
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circle_WP = next_WP;
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yaw_look_at_WP = circle_WP;
set_yaw_mode(CIRCLE_YAW);
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// set angle travelled so far to zero
circle_angle_total = 0;
// record number of desired rotations from mission command
circle_desired_rotations = command_nav_queue.p1;
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}
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// do_loiter_time - initiate loitering at a point for a given time period
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// note: caller should set yaw_mode
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static void do_loiter_time()
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{
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// set roll-pitch mode (no pilot input)
set_roll_pitch_mode(AUTO_RP);
// set throttle mode to AUTO which, if not already active, will default to hold at our current altitude
set_throttle_mode(THROTTLE_AUTO);
// set target altitude if provided
if( command_nav_queue.alt != 0 ) {
set_new_altitude(command_nav_queue.alt);
}
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// if no position specificed loiter at current location
if(command_nav_queue.lat == 0 && command_nav_queue.lng == 0) {
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set_nav_mode(NAV_LOITER);
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loiter_time = millis();
}else{
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// location specified so fly to the target location
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set_nav_mode(NAV_WP);
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// Set inav navigation target
wpinav_set_destination(command_nav_queue);
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}
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loiter_time_max = command_nav_queue.p1 * 1000; // units are (seconds)
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}
/********************************************************************************/
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// Verify Nav (Must) commands
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/********************************************************************************/
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// verify_takeoff - check if we have completed the takeoff
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static bool verify_takeoff()
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{
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// wait until we are ready!
if(g.rc_3.control_in == 0) {
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// To-Do: reset loiter target if we have not yet taken-off
// do not allow I term to build up if we have not yet taken-off
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return false;
}
// are we above our target altitude?
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return (alt_change_flag == REACHED_ALT);
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}
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// verify_land - returns true if landing has been completed
static bool verify_land()
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{
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// rely on THROTTLE_LAND mode to correctly update landing status
return ap.land_complete;
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}
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// verify_nav_wp - check if we have reached the next way point
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static bool verify_nav_wp()
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{
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// altitude checking
if( !(wp_verify_byte & NAV_ALTITUDE) ) {
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if(alt_change_flag == REACHED_ALT) {
// we have reached that altitude
wp_verify_byte |= NAV_ALTITUDE;
}
}
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// distance checking
if( !(wp_verify_byte & NAV_LOCATION) ) {
if(wp_distance <= (uint32_t)max((g.waypoint_radius * 100),0) || check_missed_wp()) {
wp_verify_byte |= NAV_LOCATION;
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}
}
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// delay checking once we've reached the location
if( !(wp_verify_byte & NAV_DELAY) && (wp_verify_byte & (NAV_LOCATION | NAV_ALTITUDE)) ) {
// start timer if necessary
if(loiter_time == 0) {
loiter_time = millis();
}
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2013-03-05 23:50:41 -04:00
// check if timer has run out
if ((millis() - loiter_time) >= loiter_time_max) {
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wp_verify_byte |= NAV_DELAY;
}
}
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if( wp_verify_byte == (NAV_LOCATION | NAV_ALTITUDE | NAV_DELAY) ) {
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gcs_send_text_fmt(PSTR("Reached Command #%i"),command_nav_index);
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copter_leds_nav_blink = 15; // Cause the CopterLEDs to blink three times to indicate waypoint reached
return true;
}else{
return false;
}
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}
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static bool verify_loiter_unlimited()
{
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if(nav_mode == NAV_WP && wp_distance <= (uint32_t)max((g.waypoint_radius * 100),0)) {
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// switch to position hold
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set_nav_mode(NAV_LOITER);
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}
return false;
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}
2011-03-02 22:32:50 -04:00
2012-12-09 02:50:50 -04:00
// verify_loiter_time - check if we have loitered long enough
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static bool verify_loiter_time()
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{
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if(nav_mode == NAV_LOITER) {
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if ((millis() - loiter_time) > loiter_time_max) {
return true;
}
}
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if(nav_mode == NAV_WP && wp_distance <= (uint32_t)max((g.waypoint_radius * 100),0)) {
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// reset our loiter time
loiter_time = millis();
// switch to position hold
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set_nav_mode(NAV_LOITER);
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}
return false;
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}
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// verify_circle - check if we have circled the point enough
static bool verify_circle()
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{
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// have we rotated around the center enough times?
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return fabs(circle_desired_rotations/M_PI) > circle_desired_rotations;
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}
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// verify_RTL - handles any state changes required to implement RTL
// do_RTL should have been called once first to initialise all variables
// returns true with RTL has completed successfully
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static bool verify_RTL()
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{
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bool retval = false;
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2012-11-29 08:08:19 -04:00
switch( rtl_state ) {
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case RTL_STATE_INITIAL_CLIMB:
// rely on verify_altitude function to update alt_change_flag when we've reached the target
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if(alt_change_flag == REACHED_ALT || alt_change_flag == DESCENDING) {
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// override target altitude to RTL altitude
set_new_altitude(get_RTL_alt());
// set navigation mode
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set_nav_mode(NAV_WP);
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// Set inav navigation target to home
wpinav_set_destination(home);
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// set yaw mode
set_yaw_mode(RTL_YAW);
// advance to next rtl state
rtl_state = RTL_STATE_RETURNING_HOME;
}
break;
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case RTL_STATE_RETURNING_HOME:
// if we've reached home initiate loiter
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if (wp_distance <= (uint32_t)max((g.waypoint_radius * 100),0) || check_missed_wp()) {
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rtl_state = RTL_STATE_LOITERING_AT_HOME;
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set_nav_mode(NAV_LOITER);
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// set loiter timer
rtl_loiter_start_time = millis();
// give pilot back control of yaw
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set_yaw_mode(YAW_HOLD);
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}
break;
case RTL_STATE_LOITERING_AT_HOME:
// check if we've loitered long enough
if( millis() - rtl_loiter_start_time > (uint32_t)g.rtl_loiter_time.get() ) {
// initiate landing or descent
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if(g.rtl_alt_final == 0 || ap.failsafe_radio) {
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// land
do_land();
// override landing location (do_land defaults to current location)
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// To-do: ensure this location override is being sent to inav loiter controller
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set_next_WP_latlon(home.lat, home.lng);
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// update RTL state
rtl_state = RTL_STATE_LAND;
}else{
// descend
if(current_loc.alt > g.rtl_alt_final) {
set_new_altitude(g.rtl_alt_final);
}
// update RTL state
rtl_state = RTL_STATE_FINAL_DESCENT;
}
}
break;
case RTL_STATE_FINAL_DESCENT:
// rely on altitude check to confirm we have reached final altitude
if(current_loc.alt <= g.rtl_alt_final || alt_change_flag == REACHED_ALT) {
// switch to regular loiter mode
set_mode(LOITER);
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// set loiter target to home position
loiter_set_target(0,0);
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// override altitude to RTL altitude
set_new_altitude(g.rtl_alt_final);
retval = true;
}
break;
case RTL_STATE_LAND:
// rely on verify_land to return correct status
retval = verify_land();
break;
default:
// this should never happen
// TO-DO: log an error
retval = true;
break;
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}
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// true is returned if we've successfully completed RTL
return retval;
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}
/********************************************************************************/
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// Condition (May) commands
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/********************************************************************************/
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static void do_wait_delay()
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{
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//cliSerial->print("dwd ");
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condition_start = millis();
condition_value = command_cond_queue.lat * 1000; // convert to milliseconds
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//cliSerial->println(condition_value,DEC);
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}
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static void do_change_alt()
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{
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// set throttle mode to AUTO
set_throttle_mode(THROTTLE_AUTO);
// set altitude target
set_new_altitude(command_cond_queue.alt);
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}
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static void do_within_distance()
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{
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condition_value = command_cond_queue.lat * 100;
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}
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static void do_yaw()
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{
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// get final angle, 1 = Relative, 0 = Absolute
if( command_cond_queue.lng == 0 ) {
// absolute angle
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yaw_look_at_heading = wrap_360_cd(command_cond_queue.alt * 100);
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}else{
// relative angle
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yaw_look_at_heading = wrap_360_cd(nav_yaw + command_cond_queue.alt * 100);
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}
2012-08-21 23:19:50 -03:00
2012-12-08 01:23:32 -04:00
// get turn speed
if( command_cond_queue.lat == 0 ) {
// default to regular auto slew rate
yaw_look_at_heading_slew = AUTO_YAW_SLEW_RATE;
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}else{
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int32_t turn_rate = (wrap_180_cd(yaw_look_at_heading - nav_yaw) / 100) / command_cond_queue.lat;
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yaw_look_at_heading_slew = constrain(turn_rate, 1, 360); // deg / sec
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}
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// set yaw mode
set_yaw_mode(YAW_LOOK_AT_HEADING);
// TO-DO: restore support for clockwise / counter clockwise rotation held in command_cond_queue.p1
// command_cond_queue.p1; // 0 = undefined, 1 = clockwise, -1 = counterclockwise
2011-03-02 22:32:50 -04:00
}
2011-03-26 03:35:52 -03:00
2011-03-13 03:25:38 -03:00
/********************************************************************************/
// Verify Condition (May) commands
/********************************************************************************/
2011-07-17 07:32:00 -03:00
static bool verify_wait_delay()
2011-03-02 22:32:50 -04:00
{
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//cliSerial->print("vwd");
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if (millis() - condition_start > (uint32_t)max(condition_value,0)) {
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//cliSerial->println("y");
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condition_value = 0;
return true;
}
2012-11-21 02:08:03 -04:00
//cliSerial->println("n");
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return false;
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}
2011-02-24 01:56:59 -04:00
2011-07-17 07:32:00 -03:00
static bool verify_change_alt()
2011-03-02 22:32:50 -04:00
{
2013-02-04 11:45:31 -04:00
// rely on alt change flag
return (alt_change_flag == REACHED_ALT);
2011-02-24 01:56:59 -04:00
}
2011-07-17 07:32:00 -03:00
static bool verify_within_distance()
2011-03-02 22:32:50 -04:00
{
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//cliSerial->printf("cond dist :%d\n", (int)condition_value);
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if (wp_distance < max(condition_value,0)) {
2012-08-21 23:19:50 -03:00
condition_value = 0;
return true;
}
return false;
2011-03-02 22:32:50 -04:00
}
2012-12-08 01:23:32 -04:00
// verify_yaw - return true if we have reached the desired heading
2011-07-17 07:32:00 -03:00
static bool verify_yaw()
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{
2013-03-28 23:14:31 -03:00
if( labs(wrap_180_cd(ahrs.yaw_sensor-yaw_look_at_heading)) <= 200 ) {
2012-08-21 23:19:50 -03:00
return true;
}else{
return false;
}
2011-03-02 22:32:50 -04:00
}
2012-07-24 23:02:54 -03:00
// verify_nav_roi - verifies that actions required by MAV_CMD_NAV_ROI have completed
// we assume the camera command has been successfully implemented by the do_nav_roi command
// so all we need to check is whether we needed to yaw the copter (due to the mount type) and
// whether that yaw has completed
// TO-DO: add support for other features of MAV_NAV_ROI including pointing at a given waypoint
static bool verify_nav_roi()
{
#if MOUNT == ENABLED
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// check if mount type requires us to rotate the quad
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if( camera_mount.get_mount_type() != AP_Mount::k_pan_tilt && camera_mount.get_mount_type() != AP_Mount::k_pan_tilt_roll ) {
2012-08-21 23:19:50 -03:00
// ensure yaw has gotten to within 2 degrees of the target
2013-03-28 23:14:31 -03:00
if( labs(wrap_180_cd(ahrs.yaw_sensor-yaw_look_at_WP_bearing)) <= 200 ) {
2012-08-21 23:19:50 -03:00
return true;
}else{
return false;
}
}else{
// if no rotation required, assume the camera instruction was implemented immediately
return true;
}
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#else
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// if we have no camera mount simply check we've reached the desired yaw
// ensure yaw has gotten to within 2 degrees of the target
2013-03-28 23:14:31 -03:00
if( labs(wrap_180_cd(ahrs.yaw_sensor-yaw_look_at_WP_bearing)) <= 200 ) {
2012-08-21 23:19:50 -03:00
return true;
}else{
return false;
}
2012-07-24 23:02:54 -03:00
#endif
}
2011-03-02 22:32:50 -04:00
/********************************************************************************/
2011-04-03 18:11:14 -03:00
// Do (Now) commands
2011-03-02 22:32:50 -04:00
/********************************************************************************/
2011-09-24 13:49:11 -03:00
static void do_change_speed()
{
2012-08-21 23:19:50 -03:00
g.waypoint_speed_max = command_cond_queue.p1 * 100;
2011-09-24 13:49:11 -03:00
}
2011-07-17 07:32:00 -03:00
static void do_jump()
2011-03-13 03:25:38 -03:00
{
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// Used to track the state of the jump command in Mission scripting
// -10 is a value that means the register is unused
// when in use, it contains the current remaining jumps
static int8_t jump = -10; // used to track loops in jump command
2012-01-03 14:21:52 -04:00
2012-11-21 02:08:03 -04:00
//cliSerial->printf("do Jump: %d\n", jump);
2011-11-17 01:28:56 -04:00
2012-08-21 23:19:50 -03:00
if(jump == -10) {
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//cliSerial->printf("Fresh Jump\n");
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// we use a locally stored index for jump
jump = command_cond_queue.lat;
}
2012-11-21 02:08:03 -04:00
//cliSerial->printf("Jumps left: %d\n",jump);
2011-03-13 03:25:38 -03:00
2012-08-21 23:19:50 -03:00
if(jump > 0) {
2012-11-21 02:08:03 -04:00
//cliSerial->printf("Do Jump to %d\n",command_cond_queue.p1);
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jump--;
change_command(command_cond_queue.p1);
2011-09-24 21:40:29 -03:00
2012-08-21 23:19:50 -03:00
} else if (jump == 0) {
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//cliSerial->printf("Did last jump\n");
2012-08-21 23:19:50 -03:00
// we're done, move along
jump = -11;
2011-09-24 21:40:29 -03:00
2012-08-21 23:19:50 -03:00
} else if (jump == -1) {
2012-11-21 02:08:03 -04:00
//cliSerial->printf("jumpForever\n");
2012-08-21 23:19:50 -03:00
// repeat forever
change_command(command_cond_queue.p1);
}
2011-03-13 03:25:38 -03:00
}
2011-07-17 07:32:00 -03:00
static void do_set_home()
2011-03-02 22:32:50 -04:00
{
2012-08-21 23:19:50 -03:00
if(command_cond_queue.p1 == 1) {
init_home();
} else {
home.id = MAV_CMD_NAV_WAYPOINT;
home.lng = command_cond_queue.lng; // Lon * 10**7
home.lat = command_cond_queue.lat; // Lat * 10**7
home.alt = 0;
2012-11-10 01:55:51 -04:00
//home_is_set = true;
set_home_is_set(true);
2012-08-21 23:19:50 -03:00
}
2011-03-02 22:32:50 -04:00
}
2011-07-17 07:32:00 -03:00
static void do_set_servo()
2011-03-02 22:32:50 -04:00
{
2012-12-06 23:58:44 -04:00
uint8_t channel_num = 0xff;
2012-12-06 07:18:33 -04:00
switch( command_cond_queue.p1 ) {
case 1:
channel_num = CH_1;
break;
case 2:
channel_num = CH_2;
break;
case 3:
channel_num = CH_3;
break;
case 4:
channel_num = CH_4;
break;
case 5:
channel_num = CH_5;
break;
case 6:
channel_num = CH_6;
break;
case 7:
channel_num = CH_7;
break;
case 8:
channel_num = CH_8;
break;
case 9:
// not used
break;
case 10:
channel_num = CH_10;
break;
case 11:
channel_num = CH_11;
break;
}
// send output to channel
2012-12-06 23:58:44 -04:00
if (channel_num != 0xff) {
2012-12-12 21:25:09 -04:00
hal.rcout->enable_ch(channel_num);
hal.rcout->write(channel_num, command_cond_queue.alt);
2012-12-06 07:18:33 -04:00
}
2011-03-02 22:32:50 -04:00
}
2011-07-17 07:32:00 -03:00
static void do_set_relay()
2011-03-02 22:32:50 -04:00
{
2012-08-21 23:19:50 -03:00
if (command_cond_queue.p1 == 1) {
relay.on();
} else if (command_cond_queue.p1 == 0) {
relay.off();
}else{
relay.toggle();
}
2011-03-13 03:25:38 -03:00
}
2011-07-17 07:32:00 -03:00
static void do_repeat_servo()
2011-03-13 03:25:38 -03:00
{
2012-08-21 23:19:50 -03:00
event_id = command_cond_queue.p1 - 1;
if(command_cond_queue.p1 >= CH_5 + 1 && command_cond_queue.p1 <= CH_8 + 1) {
event_timer = 0;
event_value = command_cond_queue.alt;
event_repeat = command_cond_queue.lat * 2;
2013-01-10 14:42:24 -04:00
event_delay = command_cond_queue.lng * 500.0f; // /2 (half cycle time) * 1000 (convert to milliseconds)
2012-08-21 23:19:50 -03:00
switch(command_cond_queue.p1) {
case CH_5:
event_undo_value = g.rc_5.radio_trim;
break;
case CH_6:
event_undo_value = g.rc_6.radio_trim;
break;
case CH_7:
event_undo_value = g.rc_7.radio_trim;
break;
case CH_8:
event_undo_value = g.rc_8.radio_trim;
break;
}
update_events();
}
2011-03-13 03:25:38 -03:00
}
2011-07-17 07:32:00 -03:00
static void do_repeat_relay()
2011-03-13 03:25:38 -03:00
{
2012-08-21 23:19:50 -03:00
event_id = RELAY_TOGGLE;
event_timer = 0;
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event_delay = command_cond_queue.lat * 500.0f; // /2 (half cycle time) * 1000 (convert to milliseconds)
2012-08-21 23:19:50 -03:00
event_repeat = command_cond_queue.alt * 2;
update_events();
2011-03-19 07:14:15 -03:00
}
2012-07-24 23:02:54 -03:00
// do_nav_roi - starts actions required by MAV_CMD_NAV_ROI
// this involves either moving the camera to point at the ROI (region of interest)
// and possibly rotating the copter to point at the ROI if our mount type does not support a yaw feature
// Note: the ROI should already be in the command_nav_queue global variable
// TO-DO: add support for other features of MAV_NAV_ROI including pointing at a given waypoint
static void do_nav_roi()
{
#if MOUNT == ENABLED
2012-08-21 23:19:50 -03:00
// check if mount type requires us to rotate the quad
2012-10-08 00:31:10 -03:00
if( camera_mount.get_mount_type() != AP_Mount::k_pan_tilt && camera_mount.get_mount_type() != AP_Mount::k_pan_tilt_roll ) {
2012-12-08 01:23:32 -04:00
yaw_look_at_WP = command_nav_queue;
set_yaw_mode(YAW_LOOK_AT_LOCATION);
2012-08-21 23:19:50 -03:00
}
// send the command to the camera mount
camera_mount.set_roi_cmd(&command_nav_queue);
// TO-DO: expand handling of the do_nav_roi to support all modes of the MAVLink. Currently we only handle mode 4 (see below)
// 0: do nothing
// 1: point at next waypoint
// 2: point at a waypoint taken from WP# parameter (2nd parameter?)
// 3: point at a location given by alt, lon, lat parameters
// 4: point at a target given a target id (can't be implmented)
2012-07-24 23:02:54 -03:00
#else
2012-12-08 01:23:32 -04:00
// if we have no camera mount aim the quad at the location
yaw_look_at_WP = command_nav_queue;
set_yaw_mode(YAW_LOOK_AT_LOCATION);
2012-07-24 23:02:54 -03:00
#endif
}
2012-12-06 10:48:30 -04:00
// do_take_picture - take a picture with the camera library
static void do_take_picture()
{
2012-12-06 11:57:08 -04:00
#if CAMERA == ENABLED
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camera.trigger_pic();
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if (g.log_bitmask & MASK_LOG_CAMERA) {
Log_Write_Camera();
}
#endif
2012-12-06 10:48:30 -04:00
}