/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- #define CONTROL_SWITCH_COUNTER 20 // 20 iterations at 100hz (i.e. 2/10th of a second) at a new switch position will cause flight mode change static void read_control_switch() { static uint8_t switch_counter = 0; uint8_t switchPosition = readSwitch(); // has switch moved? // ignore flight mode changes if in failsafe if (oldSwitchPosition != switchPosition && !failsafe.radio && failsafe.radio_counter == 0) { switch_counter++; if(switch_counter >= CONTROL_SWITCH_COUNTER) { oldSwitchPosition = switchPosition; switch_counter = 0; // set flight mode and simple mode setting if (set_mode(flight_modes[switchPosition])) { if(g.ch7_option != AUX_SWITCH_SIMPLE_MODE && g.ch8_option != AUX_SWITCH_SIMPLE_MODE && g.ch7_option != AUX_SWITCH_SUPERSIMPLE_MODE && g.ch8_option != AUX_SWITCH_SUPERSIMPLE_MODE) { // set Simple mode using stored paramters from Mission planner // rather than by the control switch if (BIT_IS_SET(g.super_simple, switchPosition)) { set_simple_mode(2); }else{ set_simple_mode(BIT_IS_SET(g.simple_modes, switchPosition)); } } } } }else{ // reset switch_counter if there's been no change // we don't want 10 intermittant blips causing a flight mode change switch_counter = 0; } } static uint8_t readSwitch(void){ int16_t pulsewidth = g.rc_5.radio_in; // default for Arducopter if (pulsewidth < 1231) return 0; if (pulsewidth < 1361) return 1; if (pulsewidth < 1491) return 2; if (pulsewidth < 1621) return 3; if (pulsewidth < 1750) return 4; // Software Manual return 5; // Hardware Manual } static void reset_control_switch() { oldSwitchPosition = -1; read_control_switch(); } // read_3pos_switch static uint8_t read_3pos_switch(int16_t radio_in){ if (radio_in < AUX_SWITCH_PWM_TRIGGER_LOW) return AUX_SWITCH_LOW; // switch is in low position if (radio_in > AUX_SWITCH_PWM_TRIGGER_HIGH) return AUX_SWITCH_HIGH; // switch is in high position return AUX_SWITCH_MIDDLE; // switch is in middle position } // read_aux_switches - checks aux switch positions and invokes configured actions static void read_aux_switches() { uint8_t switch_position; // exit immediately during radio failsafe if (failsafe.radio || failsafe.radio_counter != 0) { return; } // check if ch7 switch has changed position switch_position = read_3pos_switch(g.rc_7.radio_in); if (ap.CH7_flag != switch_position) { // set the CH7 flag ap.CH7_flag = switch_position; // invoke the appropriate function do_aux_switch_function(g.ch7_option, ap.CH7_flag); } // check if Ch8 switch has changed position switch_position = read_3pos_switch(g.rc_8.radio_in); if (ap.CH8_flag != switch_position) { // set the CH8 flag ap.CH8_flag = switch_position; // invoke the appropriate function do_aux_switch_function(g.ch8_option, ap.CH8_flag); } } // init_aux_switches - invoke configured actions at start-up for aux function where it is safe to do so static void init_aux_switches() { // set the CH7 flag ap.CH7_flag = read_3pos_switch(g.rc_7.radio_in); ap.CH8_flag = read_3pos_switch(g.rc_8.radio_in); // init channel 7 options switch(g.ch7_option) { case AUX_SWITCH_SIMPLE_MODE: case AUX_SWITCH_SONAR: case AUX_SWITCH_FENCE: case AUX_SWITCH_RESETTOARMEDYAW: case AUX_SWITCH_SUPERSIMPLE_MODE: case AUX_SWITCH_ACRO_TRAINER: case AUX_SWITCH_EPM: case AUX_SWITCH_SPRAYER: case AUX_SWITCH_EKF: case AUX_SWITCH_PARACHUTE_ENABLE: case AUX_SWITCH_PARACHUTE_3POS: // we trust the vehicle will be disarmed so even if switch is in release position the chute will not release case AUX_SWITCH_MISSIONRESET: do_aux_switch_function(g.ch7_option, ap.CH7_flag); break; } // init channel 8 option switch(g.ch8_option) { case AUX_SWITCH_SIMPLE_MODE: case AUX_SWITCH_SONAR: case AUX_SWITCH_FENCE: case AUX_SWITCH_RESETTOARMEDYAW: case AUX_SWITCH_SUPERSIMPLE_MODE: case AUX_SWITCH_ACRO_TRAINER: case AUX_SWITCH_EPM: case AUX_SWITCH_SPRAYER: case AUX_SWITCH_EKF: case AUX_SWITCH_PARACHUTE_ENABLE: case AUX_SWITCH_PARACHUTE_3POS: // we trust the vehicle will be disarmed so even if switch is in release position the chute will not release case AUX_SWITCH_MISSIONRESET: do_aux_switch_function(g.ch8_option, ap.CH8_flag); break; } } // do_aux_switch_function - implement the function invoked by the ch7 or ch8 switch static void do_aux_switch_function(int8_t ch_function, uint8_t ch_flag) { int8_t tmp_function = ch_function; // multi mode check if(ch_function == AUX_SWITCH_MULTI_MODE) { if (g.rc_6.radio_in < CH6_PWM_TRIGGER_LOW) { tmp_function = AUX_SWITCH_FLIP; }else if (g.rc_6.radio_in > CH6_PWM_TRIGGER_HIGH) { tmp_function = AUX_SWITCH_SAVE_WP; }else{ tmp_function = AUX_SWITCH_RTL; } } switch(tmp_function) { case AUX_SWITCH_FLIP: // flip if switch is on, positive throttle and we're actually flying if(ch_flag == AUX_SWITCH_HIGH) { set_mode(FLIP); }else{ flip_stop(); } break; case AUX_SWITCH_SIMPLE_MODE: // low = simple mode off, middle or high position turns simple mode on set_simple_mode(ch_flag == AUX_SWITCH_HIGH || ch_flag == AUX_SWITCH_MIDDLE); break; case AUX_SWITCH_SUPERSIMPLE_MODE: // low = simple mode off, middle = simple mode, high = super simple mode set_simple_mode(ch_flag); break; case AUX_SWITCH_RTL: if (ch_flag == AUX_SWITCH_HIGH) { // engage RTL (if not possible we remain in current flight mode) set_mode(RTL); }else{ // return to flight mode switch's flight mode if we are currently in RTL if (control_mode == RTL) { reset_control_switch(); } } break; case AUX_SWITCH_SAVE_TRIM: if ((ch_flag == AUX_SWITCH_HIGH) && (control_mode <= ACRO) && (g.rc_3.control_in == 0)) { save_trim(); } break; case AUX_SWITCH_SAVE_WP: // save waypoint when switch is brought high if (ch_flag == AUX_SWITCH_HIGH) { // do not allow saving new waypoints while we're in auto or disarmed if(control_mode == AUTO || !motors.armed()) { return; } // do not allow saving the first waypoint with zero throttle if((mission.num_commands() == 0) && (g.rc_3.control_in == 0)){ return; } // create new mission command AP_Mission::Mission_Command cmd = {}; // if the mission is empty save a takeoff command if(mission.num_commands() == 0) { // set our location ID to 16, MAV_CMD_NAV_WAYPOINT cmd.id = MAV_CMD_NAV_TAKEOFF; cmd.content.location.options = 0; cmd.p1 = 0; cmd.content.location.lat = 0; cmd.content.location.lng = 0; cmd.content.location.alt = max(current_loc.alt,100); // use the current altitude for the target alt for takeoff. // only altitude will matter to the AP mission script for takeoff. if(mission.add_cmd(cmd)) { // log event Log_Write_Event(DATA_SAVEWP_ADD_WP); } } // set new waypoint to current location cmd.content.location = current_loc; // if throttle is above zero, create waypoint command if(g.rc_3.control_in > 0) { cmd.id = MAV_CMD_NAV_WAYPOINT; }else{ // with zero throttle, create LAND command cmd.id = MAV_CMD_NAV_LAND; } // save command if(mission.add_cmd(cmd)) { // log event Log_Write_Event(DATA_SAVEWP_ADD_WP); } } break; #if CAMERA == ENABLED case AUX_SWITCH_CAMERA_TRIGGER: if (ch_flag == AUX_SWITCH_HIGH) { do_take_picture(); } break; #endif case AUX_SWITCH_SONAR: // enable or disable the sonar if (ch_flag == AUX_SWITCH_HIGH) { g.sonar_enabled = true; }else{ g.sonar_enabled = false; } break; #if AC_FENCE == ENABLED case AUX_SWITCH_FENCE: // enable or disable the fence if (ch_flag == AUX_SWITCH_HIGH) { fence.enable(true); Log_Write_Event(DATA_FENCE_ENABLE); }else{ fence.enable(false); Log_Write_Event(DATA_FENCE_DISABLE); } break; #endif // To-Do: add back support for this feature //case AUX_SWITCH_RESETTOARMEDYAW: // if (ch_flag == AUX_SWITCH_HIGH) { // set_yaw_mode(YAW_RESETTOARMEDYAW); // }else{ // set_yaw_mode(YAW_HOLD); // } // break; case AUX_SWITCH_ACRO_TRAINER: switch(ch_flag) { case AUX_SWITCH_LOW: g.acro_trainer = ACRO_TRAINER_DISABLED; Log_Write_Event(DATA_ACRO_TRAINER_DISABLED); break; case AUX_SWITCH_MIDDLE: g.acro_trainer = ACRO_TRAINER_LEVELING; Log_Write_Event(DATA_ACRO_TRAINER_LEVELING); break; case AUX_SWITCH_HIGH: g.acro_trainer = ACRO_TRAINER_LIMITED; Log_Write_Event(DATA_ACRO_TRAINER_LIMITED); break; } break; #if EPM_ENABLED == ENABLED case AUX_SWITCH_EPM: switch(ch_flag) { case AUX_SWITCH_LOW: epm.off(); Log_Write_Event(DATA_EPM_OFF); break; case AUX_SWITCH_MIDDLE: epm.neutral(); Log_Write_Event(DATA_EPM_NEUTRAL); break; case AUX_SWITCH_HIGH: epm.on(); Log_Write_Event(DATA_EPM_ON); break; } break; #endif #if SPRAYER == ENABLED case AUX_SWITCH_SPRAYER: sprayer.enable(ch_flag == AUX_SWITCH_HIGH); // if we are disarmed the pilot must want to test the pump sprayer.test_pump((ch_flag == AUX_SWITCH_HIGH) && !motors.armed()); break; #endif case AUX_SWITCH_AUTO: if (ch_flag == AUX_SWITCH_HIGH) { set_mode(AUTO); }else{ // return to flight mode switch's flight mode if we are currently in AUTO if (control_mode == AUTO) { reset_control_switch(); } } break; #if AUTOTUNE_ENABLED == ENABLED case AUX_SWITCH_AUTOTUNE: // turn on auto tuner switch(ch_flag) { case AUX_SWITCH_LOW: case AUX_SWITCH_MIDDLE: // stop the autotune and return to original gains autotune_stop(); // restore flight mode based on flight mode switch position if (control_mode == AUTOTUNE) { reset_control_switch(); } break; case AUX_SWITCH_HIGH: // start an autotuning session autotune_start(); break; } break; #endif case AUX_SWITCH_LAND: if (ch_flag == AUX_SWITCH_HIGH) { set_mode(LAND); }else{ // return to flight mode switch's flight mode if we are currently in LAND if (control_mode == LAND) { reset_control_switch(); } } break; #if AP_AHRS_NAVEKF_AVAILABLE case AUX_SWITCH_EKF: ahrs.set_ekf_use(ch_flag==AUX_SWITCH_HIGH); break; #endif #if PARACHUTE == ENABLED case AUX_SWITCH_PARACHUTE_ENABLE: // Parachute enable/disable parachute.enabled(ch_flag == AUX_SWITCH_HIGH); break; case AUX_SWITCH_PARACHUTE_RELEASE: if (ch_flag == AUX_SWITCH_HIGH) { parachute_manual_release(); } break; case AUX_SWITCH_PARACHUTE_3POS: // Parachute disable, enable, release with 3 position switch switch (ch_flag) { case AUX_SWITCH_LOW: parachute.enabled(false); Log_Write_Event(DATA_PARACHUTE_DISABLED); break; case AUX_SWITCH_MIDDLE: parachute.enabled(true); Log_Write_Event(DATA_PARACHUTE_ENABLED); break; case AUX_SWITCH_HIGH: parachute.enabled(true); parachute_manual_release(); break; } break; #endif case AUX_SWITCH_MISSIONRESET: if (ch_flag == AUX_SWITCH_HIGH) { mission.reset(); } break; } } // save_trim - adds roll and pitch trims from the radio to ahrs static void save_trim() { // save roll and pitch trim float roll_trim = ToRad((float)g.rc_1.control_in/100.0f); float pitch_trim = ToRad((float)g.rc_2.control_in/100.0f); ahrs.add_trim(roll_trim, pitch_trim); Log_Write_Event(DATA_SAVE_TRIM); gcs_send_text_P(SEVERITY_HIGH, PSTR("Trim saved")); } // auto_trim - slightly adjusts the ahrs.roll_trim and ahrs.pitch_trim towards the current stick positions // meant to be called continuously while the pilot attempts to keep the copter level static void auto_trim() { if(auto_trim_counter > 0) { auto_trim_counter--; // flash the leds AP_Notify::flags.save_trim = true; // calculate roll trim adjustment float roll_trim_adjustment = ToRad((float)g.rc_1.control_in / 4000.0f); // calculate pitch trim adjustment float pitch_trim_adjustment = ToRad((float)g.rc_2.control_in / 4000.0f); // make sure accelerometer values impact attitude quickly ahrs.set_fast_gains(true); // add trim to ahrs object // save to eeprom on last iteration ahrs.add_trim(roll_trim_adjustment, pitch_trim_adjustment, (auto_trim_counter == 0)); // on last iteration restore leds and accel gains to normal if(auto_trim_counter == 0) { ahrs.set_fast_gains(false); AP_Notify::flags.save_trim = false; } } }