/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- #define CONTROL_SWITCH_COUNTER 10 // 10 iterations at 100hz (i.e. 1/10th of a second) at a new switch position will cause flight mode change static void read_control_switch() { static uint8_t switch_counter = 0; byte switchPosition = readSwitch(); if (oldSwitchPosition != switchPosition) { switch_counter++; if(switch_counter >= CONTROL_SWITCH_COUNTER) { oldSwitchPosition = switchPosition; switch_counter = 0; // ignore flight mode changes if in failsafe if( !ap.failsafe ) { set_mode(flight_modes[switchPosition]); if(g.ch7_option != CH7_SIMPLE_MODE) { // set Simple mode using stored paramters from Mission planner // rather than by the control switch set_simple_mode(g.simple_modes & (1 << 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 byte readSwitch(void){ int16_t pulsewidth = g.rc_5.radio_in; // default for Arducopter if (pulsewidth > 1230 && pulsewidth <= 1360) return 1; if (pulsewidth > 1360 && pulsewidth <= 1490) return 2; if (pulsewidth > 1490 && pulsewidth <= 1620) return 3; if (pulsewidth > 1620 && pulsewidth <= 1749) return 4; if (pulsewidth >= 1750) return 5; return 0; } static void reset_control_switch() { oldSwitchPosition = -1; read_control_switch(); } // read at 10 hz // set this to your trainer switch static void read_trim_switch() { // return immediately if the CH7 switch has not changed position if (ap_system.CH7_flag == (g.rc_7.radio_in >= CH7_PWM_TRIGGER)) { return; } // set the ch7 flag ap_system.CH7_flag = (g.rc_7.radio_in >= CH7_PWM_TRIGGER); switch(g.ch7_option) { case CH7_FLIP: // flip if switch is on, positive throttle and we're actually flying if(ap_system.CH7_flag && g.rc_3.control_in >= 0 && ap.takeoff_complete) { init_flip(); } break; case CH7_SIMPLE_MODE: set_simple_mode(ap_system.CH7_flag); break; case CH7_RTL: if (ap_system.CH7_flag) { // engage RTL set_mode(RTL); }else{ // disengage RTL to previous flight mode if we are currently in RTL or loiter if (control_mode == RTL || control_mode == LOITER) { reset_control_switch(); } } break; case CH7_SAVE_TRIM: if(ap_system.CH7_flag && control_mode <= ACRO && g.rc_3.control_in == 0) { save_trim_counter = 15; } break; case CH7_SAVE_WP: // save when CH7 switch is switched off if (ap_system.CH7_flag == false) { // if in auto mode, reset the mission if(control_mode == AUTO) { CH7_wp_index = 0; g.command_total.set_and_save(1); set_mode(RTL); return; } if(CH7_wp_index == 0) { // this is our first WP, let's save WP 1 as a takeoff // increment index to WP index of 1 (home is stored at 0) CH7_wp_index = 1; Location temp = home; // set our location ID to 16, MAV_CMD_NAV_WAYPOINT temp.id = MAV_CMD_NAV_TAKEOFF; temp.alt = current_loc.alt; // save command: // we use the current altitude to be the target for takeoff. // only altitude will matter to the AP mission script for takeoff. // If we are above the altitude, we will skip the command. set_cmd_with_index(temp, CH7_wp_index); } // increment index CH7_wp_index++; // set the next_WP (home is stored at 0) // max out at 100 since I think we need to stay under the EEPROM limit CH7_wp_index = constrain(CH7_wp_index, 1, 100); if(g.rc_3.control_in > 0) { // set our location ID to 16, MAV_CMD_NAV_WAYPOINT current_loc.id = MAV_CMD_NAV_WAYPOINT; }else{ // set our location ID to 21, MAV_CMD_NAV_LAND current_loc.id = MAV_CMD_NAV_LAND; } // save command set_cmd_with_index(current_loc, CH7_wp_index); // Cause the CopterLEDs to blink twice to indicate saved waypoint copter_leds_nav_blink = 10; } break; #if CAMERA == ENABLED case CH7_CAMERA_TRIGGER: if(ap_system.CH7_flag) { do_take_picture(); } break; #endif } } // save_trim - adds roll and pitch trims from the radio to ahrs static void save_trim() { float roll_trim, pitch_trim; if(save_trim_counter > 0) { save_trim_counter--; // first few iterations we simply flash the leds led_mode = SAVE_TRIM_LEDS; if(save_trim_counter == 1) { // save roll trim roll_trim = ToRad((float)g.rc_1.control_in/100.0); pitch_trim = ToRad((float)g.rc_2.control_in/100.0); ahrs.add_trim(roll_trim, pitch_trim); reset_control_switch(); // switch back leds to normal led_mode = NORMAL_LEDS; save_trim_counter = 0; } } }