mirror of https://github.com/ArduPilot/ardupilot
187 lines
6.1 KiB
Plaintext
187 lines
6.1 KiB
Plaintext
/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
|
|
|
|
static void read_control_switch()
|
|
{
|
|
static bool switch_debouncer = false;
|
|
|
|
byte switchPosition = readSwitch();
|
|
|
|
if (oldSwitchPosition != switchPosition) {
|
|
if(switch_debouncer) {
|
|
oldSwitchPosition = switchPosition;
|
|
switch_debouncer = false;
|
|
|
|
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
|
|
//ap.simple_mode = (g.simple_modes & (1 << switchPosition));
|
|
set_simple_mode(g.simple_modes & (1 << switchPosition));
|
|
}
|
|
}else{
|
|
switch_debouncer = true;
|
|
}
|
|
}
|
|
}
|
|
|
|
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; // Software Manual
|
|
if (pulsewidth >= 1750) return 5; // Hardware Manual
|
|
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()
|
|
{
|
|
int8_t option;
|
|
|
|
if(g.ch7_option == CH7_MULTI_MODE) {
|
|
if (g.rc_6.radio_in < CH_6_PWM_TRIGGER_LOW) {
|
|
option = CH7_FLIP;
|
|
}else if (g.rc_6.radio_in > CH_6_PWM_TRIGGER_HIGH) {
|
|
option = CH7_SAVE_WP;
|
|
}else{
|
|
option = CH7_RTL;
|
|
}
|
|
}else{
|
|
option = g.ch7_option;
|
|
}
|
|
|
|
if(option == CH7_SIMPLE_MODE) {
|
|
//ap.simple_mode = (g.rc_7.radio_in > CH_7_PWM_TRIGGER);
|
|
set_simple_mode(g.rc_7.radio_in > CH_7_PWM_TRIGGER);
|
|
|
|
}else if (option == CH7_FLIP) {
|
|
if (ap_system.CH7_flag == false && g.rc_7.radio_in > CH_7_PWM_TRIGGER) {
|
|
ap_system.CH7_flag = true;
|
|
|
|
// don't flip if we accidentally engaged flip, but didn't notice and tried to takeoff
|
|
if(g.rc_3.control_in != 0 && ap.takeoff_complete) {
|
|
init_flip();
|
|
}
|
|
}
|
|
if (ap_system.CH7_flag == true && g.rc_7.control_in < 800) {
|
|
ap_system.CH7_flag = false;
|
|
}
|
|
|
|
}else if (option == CH7_RTL) {
|
|
if (ap_system.CH7_flag == false && g.rc_7.radio_in > CH_7_PWM_TRIGGER) {
|
|
ap_system.CH7_flag = true;
|
|
set_mode(RTL);
|
|
}
|
|
|
|
if (ap_system.CH7_flag == true && g.rc_7.control_in < 800) {
|
|
ap_system.CH7_flag = false;
|
|
if (control_mode == RTL || control_mode == LOITER) {
|
|
reset_control_switch();
|
|
}
|
|
}
|
|
|
|
}else if (option == CH7_SAVE_WP) {
|
|
if (g.rc_7.radio_in > CH_7_PWM_TRIGGER) { // switch is engaged
|
|
ap_system.CH7_flag = true;
|
|
|
|
}else{ // switch is disengaged
|
|
if(ap_system.CH7_flag) {
|
|
ap_system.CH7_flag = false;
|
|
|
|
if(control_mode == AUTO) {
|
|
// reset the mission
|
|
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);
|
|
|
|
copter_leds_nav_blink = 10; // Cause the CopterLEDs to blink twice to indicate saved waypoint
|
|
|
|
// 0 = home
|
|
// 1 = takeoff
|
|
// 2 = WP 2
|
|
// 3 = command total
|
|
}
|
|
}
|
|
}else if (option == CH7_AUTO_TRIM) {
|
|
if(g.rc_7.radio_in > CH_7_PWM_TRIGGER && control_mode <= ACRO && g.rc_3.control_in == 0) {
|
|
save_trim_counter = 15;
|
|
}
|
|
}
|
|
}
|
|
|
|
// 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;
|
|
}
|
|
}
|
|
}
|
|
|
|
|