mirror of https://github.com/ArduPilot/ardupilot
193 lines
6.3 KiB
Plaintext
193 lines
6.3 KiB
Plaintext
/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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#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
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static void read_control_switch()
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{
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static uint8_t switch_counter = 0;
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byte switchPosition = readSwitch();
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if (oldSwitchPosition != switchPosition) {
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switch_counter++;
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if(switch_counter >= CONTROL_SWITCH_COUNTER) {
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oldSwitchPosition = switchPosition;
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switch_counter = 0;
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// ignore flight mode changes if in failsafe
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if( !ap.failsafe ) {
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set_mode(flight_modes[switchPosition]);
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if(g.ch7_option != CH7_SIMPLE_MODE) {
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// set Simple mode using stored paramters from Mission planner
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// rather than by the control switch
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set_simple_mode(g.simple_modes & (1 << switchPosition));
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}
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}
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}
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}else{
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// reset switch_counter if there's been no change
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// we don't want 10 intermittant blips causing a flight mode change
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switch_counter = 0;
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}
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}
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static byte readSwitch(void){
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int16_t pulsewidth = g.rc_5.radio_in; // default for Arducopter
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if (pulsewidth > 1230 && pulsewidth <= 1360) return 1;
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if (pulsewidth > 1360 && pulsewidth <= 1490) return 2;
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if (pulsewidth > 1490 && pulsewidth <= 1620) return 3;
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if (pulsewidth > 1620 && pulsewidth <= 1749) return 4;
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if (pulsewidth >= 1750) return 5;
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return 0;
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}
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static void reset_control_switch()
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{
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oldSwitchPosition = -1;
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read_control_switch();
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}
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// read at 10 hz
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// set this to your trainer switch
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static void read_trim_switch()
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{
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int8_t option;
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if(g.ch7_option == CH7_MULTI_MODE) {
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if (g.rc_6.radio_in < CH_6_PWM_TRIGGER_LOW) {
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option = CH7_FLIP;
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}else if (g.rc_6.radio_in > CH_6_PWM_TRIGGER_HIGH) {
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option = CH7_SAVE_WP;
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}else{
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option = CH7_RTL;
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}
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}else{
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option = g.ch7_option;
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}
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if(option == CH7_SIMPLE_MODE) {
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//ap.simple_mode = (g.rc_7.radio_in > CH_7_PWM_TRIGGER);
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set_simple_mode(g.rc_7.radio_in > CH_7_PWM_TRIGGER);
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}else if (option == CH7_FLIP) {
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if (ap_system.CH7_flag == false && g.rc_7.radio_in > CH_7_PWM_TRIGGER) {
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ap_system.CH7_flag = true;
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// don't flip if we accidentally engaged flip, but didn't notice and tried to takeoff
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if(g.rc_3.control_in != 0 && ap.takeoff_complete) {
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init_flip();
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}
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}
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if (ap_system.CH7_flag == true && g.rc_7.control_in < 800) {
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ap_system.CH7_flag = false;
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}
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}else if (option == CH7_RTL) {
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if (ap_system.CH7_flag == false && g.rc_7.radio_in > CH_7_PWM_TRIGGER) {
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ap_system.CH7_flag = true;
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set_mode(RTL);
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}
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if (ap_system.CH7_flag == true && g.rc_7.control_in < 800) {
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ap_system.CH7_flag = false;
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if (control_mode == RTL || control_mode == LOITER) {
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reset_control_switch();
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}
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}
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}else if (option == CH7_SAVE_WP) {
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if (g.rc_7.radio_in > CH_7_PWM_TRIGGER) { // switch is engaged
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ap_system.CH7_flag = true;
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}else{ // switch is disengaged
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if(ap_system.CH7_flag) {
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ap_system.CH7_flag = false;
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if(control_mode == AUTO) {
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// reset the mission
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CH7_wp_index = 0;
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g.command_total.set_and_save(1);
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set_mode(RTL);
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return;
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}
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if(CH7_wp_index == 0) {
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// this is our first WP, let's save WP 1 as a takeoff
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// increment index to WP index of 1 (home is stored at 0)
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CH7_wp_index = 1;
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Location temp = home;
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// set our location ID to 16, MAV_CMD_NAV_WAYPOINT
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temp.id = MAV_CMD_NAV_TAKEOFF;
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temp.alt = current_loc.alt;
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// save command:
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// we use the current altitude to be the target for takeoff.
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// only altitude will matter to the AP mission script for takeoff.
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// If we are above the altitude, we will skip the command.
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set_cmd_with_index(temp, CH7_wp_index);
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}
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// increment index
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CH7_wp_index++;
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// set the next_WP (home is stored at 0)
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// max out at 100 since I think we need to stay under the EEPROM limit
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CH7_wp_index = constrain(CH7_wp_index, 1, 100);
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if(g.rc_3.control_in > 0) {
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// set our location ID to 16, MAV_CMD_NAV_WAYPOINT
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current_loc.id = MAV_CMD_NAV_WAYPOINT;
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}else{
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// set our location ID to 21, MAV_CMD_NAV_LAND
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current_loc.id = MAV_CMD_NAV_LAND;
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}
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// save command
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set_cmd_with_index(current_loc, CH7_wp_index);
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copter_leds_nav_blink = 10; // Cause the CopterLEDs to blink twice to indicate saved waypoint
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// 0 = home
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// 1 = takeoff
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// 2 = WP 2
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// 3 = command total
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}
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}
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}else if (option == CH7_AUTO_TRIM) {
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if(g.rc_7.radio_in > CH_7_PWM_TRIGGER && control_mode <= ACRO && g.rc_3.control_in == 0) {
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save_trim_counter = 15;
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}
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}
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}
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// save_trim - adds roll and pitch trims from the radio to ahrs
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static void save_trim()
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{
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float roll_trim, pitch_trim;
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if(save_trim_counter > 0) {
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save_trim_counter--;
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// first few iterations we simply flash the leds
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led_mode = SAVE_TRIM_LEDS;
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if(save_trim_counter == 1) {
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// save roll trim
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roll_trim = ToRad((float)g.rc_1.control_in/100.0);
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pitch_trim = ToRad((float)g.rc_2.control_in/100.0);
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ahrs.add_trim(roll_trim, pitch_trim);
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reset_control_switch();
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// switch back leds to normal
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led_mode = NORMAL_LEDS;
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save_trim_counter = 0;
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}
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}
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}
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