// called by 10 Hz loop // -------------------- void update_commands(void) { // This function loads commands into three buffers // when a new command is loaded, it is processed with process_XXX() // ---------------------------------------------------------------- if((home_is_set == false) || (control_mode != AUTO)){ return; // don't do commands } if(control_mode == AUTO){ load_next_command(); process_next_command(); } //verify_must(); //verify_may(); } void load_next_command() { // fetch next command if it's empty // -------------------------------- if(next_command.id == CMD_BLANK){ next_command = get_wp_with_index(wp_index+1); if(next_command.id != CMD_BLANK){ //Serial.print("MSG fetch found new cmd from list at index: "); //Serial.println((wp_index+1),DEC); //Serial.print("MSG cmd id: "); //Serial.println(next_command.id,DEC); } } // If the preload failed, return or just Loiter // generate a dynamic command for RTL // -------------------------------------------- if(next_command.id == CMD_BLANK){ // we are out of commands! //send_message(SEVERITY_LOW,"out of commands!"); //Serial.print("MSG out of commands, wp_index: "); //Serial.println(wp_index,DEC); switch (control_mode){ case LAND: // don't get a new command break; default: next_command = get_LOITER_home_wp(); //Serial.print("MSG Preload RTL cmd id: "); //Serial.println(next_command.id,DEC); break; } } } void process_next_command() { // these are waypoint/Must commands // --------------------------------- if (command_must_index == 0){ // no current command loaded if (next_command.id >= 0x10 && next_command.id <= 0x1F ){ increment_WP_index(); save_command_index(); // to Recover from in air Restart command_must_index = wp_index; //Serial.print("MSG new command_must_id "); //Serial.print(next_command.id,DEC); //Serial.print(" index:"); //Serial.println(command_must_index,DEC); if (log_bitmask & MASK_LOG_CMD) Log_Write_Cmd(wp_index, &next_command); process_must(); } } // these are May commands // ---------------------- if (command_may_index == 0){ if (next_command.id >= 0x20 && next_command.id <= 0x2F ){ increment_WP_index();// this command is from the command list in EEPROM command_may_index = wp_index; //Serial.print("new command_may_index "); //Serial.println(command_may_index,DEC); if (log_bitmask & MASK_LOG_CMD) Log_Write_Cmd(wp_index, &next_command); process_may(); } } // these are do it now commands // --------------------------- if (next_command.id >= 0x30){ increment_WP_index();// this command is from the command list in EEPROM if (log_bitmask & MASK_LOG_CMD) Log_Write_Cmd(wp_index, &next_command); process_now(); } } /* These functions implement the waypoint commands. */ void process_must() { //Serial.print("process must index: "); //Serial.println(command_must_index,DEC); send_message(SEVERITY_LOW,"New cmd: "); send_message(MSG_COMMAND, wp_index); // clear May indexes command_may_index = 0; command_may_ID = 0; command_must_ID = next_command.id; // invalidate command so a new one is loaded // ----------------------------------------- next_command.id = 0; // reset navigation integrators // ------------------------- reset_I(); // loads the waypoint into Next_WP struct // -------------------------------------- set_next_WP(&next_command); switch(command_must_ID){ case CMD_TAKEOFF: // TAKEOFF! takeoff_altitude = (int)next_command.alt; next_WP.lat = current_loc.lat + 10; // so we don't have bad calcs next_WP.lng = current_loc.lng + 10; // so we don't have bad calcs takeoff_complete = false; // set flag to use gps ground course during TO. IMU will be doing yaw drift correction break; case CMD_WAYPOINT: // Navigate to Waypoint break; case CMD_R_WAYPOINT: // Navigate to Waypoint next_command.lat += home.lat; // offset from home location next_command.lng += home.lng; // offset from home location // we've recalculated the WP so we need to set it again set_next_WP(&next_command); break; case CMD_LAND: // LAND to Waypoint velocity_land = 1000; next_WP.lat = current_loc.lat; next_WP.lng = current_loc.lng; next_WP.alt = home.alt; land_complete = false; // set flag to use gps ground course during TO. IMU will be doing yaw drift correction break; case CMD_ALTITUDE: // Loiter indefinitely next_WP.lat = current_loc.lat + 10; // so we don't have bad calcs next_WP.lng = current_loc.lng + 10; // so we don't have bad calcs break; case CMD_LOITER: // Loiter indefinitely break; case CMD_LOITER_N_TURNS: // Loiter N Times break; case CMD_LOITER_TIME: break; case CMD_RTL: return_to_launch(); break; } } void process_may() { //Serial.print("process_may cmd# "); //Serial.println(wp_index,DEC); command_may_ID = next_command.id; // invalidate command so a new one is loaded // ----------------------------------------- next_command.id = 0; send_message(SEVERITY_LOW,"New cmd: "); send_message(MSG_COMMAND, wp_index); // do the command // -------------- switch(command_may_ID){ case CMD_DELAY: // Navigate to Waypoint delay_start = millis(); delay_timeout = next_command.lat; break; case CMD_LAND_OPTIONS: // Land this puppy break; case CMD_ANGLE: // p1: bearing // alt: speed // lat: direction (-1,1), // lng: rel (1) abs (0) // target angle in degrees command_yaw_start = nav_yaw; // current position command_yaw_start_time = millis(); // which direction to turn // 1 = clockwise, -1 = counterclockwise command_yaw_dir = next_command.lat; // 1 = Relative or 0 = Absolute if (next_command.lng == 1) { // relative command_yaw_dir = (command_yaw_end > 0) ? 1 : -1; command_yaw_end += nav_yaw; command_yaw_end = wrap_360(command_yaw_end); } else { // absolute command_yaw_end = next_command.p1 * 100; } // if unspecified go 10° a second if(command_yaw_speed == 0) command_yaw_speed = 10; // if unspecified go clockwise if(command_yaw_dir == 0) command_yaw_dir = 1; // calculate the delta travel if(command_yaw_dir == 1){ if(command_yaw_start > command_yaw_end){ command_yaw_delta = 36000 - (command_yaw_start - command_yaw_end); }else{ command_yaw_delta = command_yaw_end - command_yaw_start; } }else{ if(command_yaw_start > command_yaw_end){ command_yaw_delta = command_yaw_start - command_yaw_end; }else{ command_yaw_delta = 36000 + (command_yaw_start - command_yaw_end); } } command_yaw_delta = wrap_360(command_yaw_delta); // rate to turn deg per second - default is ten command_yaw_speed = next_command.alt; command_yaw_time = command_yaw_delta / command_yaw_speed; //9000 turn in 10 seconds //command_yaw_time = 9000/ 10 = 900° per second break; default: break; } } void process_now() { const float t5 = 100000.0; //Serial.print("process_now cmd# "); //Serial.println(wp_index,DEC); byte id = next_command.id; // invalidate command so a new one is loaded // ----------------------------------------- next_command.id = 0; send_message(SEVERITY_LOW, "New cmd: "); send_message(MSG_COMMAND, wp_index); // do the command // -------------- switch(id){ case CMD_RESET_INDEX: init_commands(); break; case CMD_GETVAR_INDEX: // break; case CMD_SENDVAR_INDEX: // break; case CMD_TELEMETRY: // break; //case CMD_AIRSPEED_CRUISE: //airspeed_cruise = next_command.p1 * 100; // todo save to EEPROM //break; case CMD_THROTTLE_CRUISE: throttle_cruise = next_command.p1; // todo save to EEPROM break; case CMD_RESET_HOME: init_home(); break; case CMD_KP_GAIN: //kp[next_command.p1] = next_command.alt/t5; // todo save to EEPROM break; case CMD_KI_GAIN: //ki[next_command.p1] = next_command.alt/t5; // todo save to EEPROM break; case CMD_KD_GAIN: //kd[next_command.p1] = next_command.alt/t5; // todo save to EEPROM break; case CMD_KI_MAX: //integrator_max[next_command.p1] = next_command.alt/t5; // todo save to EEPROM break; //case CMD_KFF_GAIN: // kff[next_command.p1] = next_command.alt/t5; // todo save to EEPROM // break; //case CMD_RADIO_TRIM: //radio_trim[next_command.p1] = next_command.alt; //save_EEPROM_trims(); //break; //case CMD_RADIO_MAX: // radio_max[next_command.p1] = next_command.alt; // save_EEPROM_radio_minmax(); // break; //case CMD_RADIO_MIN: // radio_min[next_command.p1] = next_command.alt; // save_EEPROM_radio_minmax(); // break; case CMD_REPEAT: new_event(&next_command); break; case CMD_SERVO: APM_RC.OutputCh(next_command.p1, next_command.alt); break; case CMD_INDEX: command_must_index = 0; command_may_index = 0; wp_index = next_command.p1 - 1; break; case CMD_RELAY: if(next_command.p1 = 0){ relay_A(); }else{ relay_B(); } break; } } // Verify commands // --------------- void verify_must() { float power; switch(command_must_ID) { case CMD_ALTITUDE: if (abs(next_WP.alt - current_loc.alt) < 100){ command_must_index = 0; } break; case CMD_TAKEOFF: // Takeoff! if (current_loc.alt > (home.alt + takeoff_altitude)){ command_must_index = 0; takeoff_complete = true; } break; case CMD_LAND: // 10 - 9 = 1 velocity_land = ((old_alt - current_loc.alt) *.05) + (velocity_land * .95); old_alt = current_loc.alt; if(velocity_land == 0){ land_complete = true; command_must_index = 0; } break; case CMD_WAYPOINT: // reach a waypoint if ((wp_distance > 0) && (wp_distance <= wp_radius)) { Serial.print("MSG REACHED_WAYPOINT #"); Serial.println(command_must_index,DEC); // clear the command queue; command_must_index = 0; } // add in a more complex case // Doug to do if(loiter_sum > 300){ send_message(SEVERITY_MEDIUM,"Missed WP"); command_must_index = 0; } break; case CMD_LOITER_N_TURNS: // LOITER N times break; case CMD_LOITER_TIME: // loiter N milliseconds break; case CMD_RTL: if (wp_distance <= wp_radius) { //Serial.println("REACHED_HOME"); command_must_index = 0; } break; case CMD_LOITER: // Just plain LOITER break; case CMD_ANGLE: if((millis() - command_yaw_start_time) > command_yaw_time){ command_must_index = 0; nav_yaw = command_yaw_end; }else{ // else we need to be at a certain place // power is a ratio of the time : .5 = half done power = (float)(millis() - command_yaw_start_time) / (float)command_yaw_time; nav_yaw = command_yaw_start + ((float)command_yaw_delta * power * command_yaw_dir); } break; default: send_message(SEVERITY_HIGH,"No current Must commands"); break; } } void verify_may() { switch(command_may_ID) { case CMD_DELAY: if ((millis() - delay_start) > delay_timeout){ command_may_index = 0; delay_timeout = 0; } case CMD_LAND_OPTIONS: break; } }