mirror of https://github.com/ArduPilot/ardupilot
1219 lines
27 KiB
Plaintext
1219 lines
27 KiB
Plaintext
// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: t -*-
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// Functions called from the setup menu
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static int8_t setup_radio (uint8_t argc, const Menu::arg *argv);
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static int8_t setup_motors (uint8_t argc, const Menu::arg *argv);
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static int8_t setup_accel (uint8_t argc, const Menu::arg *argv);
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static int8_t setup_factory (uint8_t argc, const Menu::arg *argv);
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static int8_t setup_erase (uint8_t argc, const Menu::arg *argv);
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static int8_t setup_flightmodes (uint8_t argc, const Menu::arg *argv);
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static int8_t setup_pid (uint8_t argc, const Menu::arg *argv);
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static int8_t setup_frame (uint8_t argc, const Menu::arg *argv);
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static int8_t setup_current (uint8_t argc, const Menu::arg *argv);
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static int8_t setup_sonar (uint8_t argc, const Menu::arg *argv);
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static int8_t setup_compass (uint8_t argc, const Menu::arg *argv);
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//static int8_t setup_mag_offset (uint8_t argc, const Menu::arg *argv);
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static int8_t setup_declination (uint8_t argc, const Menu::arg *argv);
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static int8_t setup_show (uint8_t argc, const Menu::arg *argv);
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// Command/function table for the setup menu
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const struct Menu::command setup_menu_commands[] PROGMEM = {
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// command function called
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// ======= ===============
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{"erase", setup_erase},
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{"reset", setup_factory},
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{"pid", setup_pid},
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{"radio", setup_radio},
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{"motors", setup_motors},
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{"level", setup_accel},
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{"modes", setup_flightmodes},
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{"frame", setup_frame},
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{"current", setup_current},
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{"sonar", setup_sonar},
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{"compass", setup_compass},
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// {"mag_offset", setup_mag_offset},
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{"declination", setup_declination},
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{"show", setup_show}
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};
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// Create the setup menu object.
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MENU(setup_menu, "setup", setup_menu_commands);
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// Called from the top-level menu to run the setup menu.
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int8_t
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setup_mode(uint8_t argc, const Menu::arg *argv)
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{
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// Give the user some guidance
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Serial.printf_P(PSTR("Setup Mode\n"
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"\n"
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"IMPORTANT: if you have not previously set this system up, use the\n"
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"'reset' command to initialize the EEPROM to sensible default values\n"
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"and then the 'radio' command to configure for your radio.\n"
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"\n"));
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// Run the setup menu. When the menu exits, we will return to the main menu.
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setup_menu.run();
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}
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// Print the current configuration.
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// Called by the setup menu 'show' command.
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static int8_t
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setup_show(uint8_t argc, const Menu::arg *argv)
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{
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uint8_t i;
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// clear the area
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print_blanks(8);
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report_radio();
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report_frame();
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report_current();
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report_sonar();
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report_gains();
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report_xtrack();
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report_throttle();
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report_flight_modes();
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report_imu();
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report_compass();
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AP_Var_menu_show(argc, argv);
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return(0);
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}
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// Initialise the EEPROM to 'factory' settings (mostly defined in APM_Config.h or via defaults).
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// Called by the setup menu 'factoryreset' command.
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static int8_t
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setup_factory(uint8_t argc, const Menu::arg *argv)
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{
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uint8_t i;
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int c;
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Serial.printf_P(PSTR("\nType 'Y' and hit Enter to perform factory reset, any other key to abort:\n"));
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do {
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c = Serial.read();
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} while (-1 == c);
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if (('y' != c) && ('Y' != c))
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return(-1);
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AP_Var::erase_all();
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Serial.printf_P(PSTR("\nFACTORY RESET complete - please reset APM to continue"));
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delay(1000);
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default_log_bitmask();
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default_gains();
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for (;;) {
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}
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// note, cannot actually return here
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return(0);
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}
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// Perform radio setup.
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// Called by the setup menu 'radio' command.
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static int8_t
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setup_radio(uint8_t argc, const Menu::arg *argv)
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{
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Serial.println("\n\nRadio Setup:");
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uint8_t i;
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for(i = 0; i < 100;i++){
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delay(20);
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read_radio();
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}
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if(g.rc_1.radio_in < 500){
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while(1){
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Serial.printf_P(PSTR("\nNo radio; Check connectors."));
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delay(1000);
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// stop here
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}
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}
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g.rc_1.radio_min = g.rc_1.radio_in;
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g.rc_2.radio_min = g.rc_2.radio_in;
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g.rc_3.radio_min = g.rc_3.radio_in;
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g.rc_4.radio_min = g.rc_4.radio_in;
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g.rc_5.radio_min = g.rc_5.radio_in;
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g.rc_6.radio_min = g.rc_6.radio_in;
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g.rc_7.radio_min = g.rc_7.radio_in;
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g.rc_8.radio_min = g.rc_8.radio_in;
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g.rc_1.radio_max = g.rc_1.radio_in;
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g.rc_2.radio_max = g.rc_2.radio_in;
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g.rc_3.radio_max = g.rc_3.radio_in;
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g.rc_4.radio_max = g.rc_4.radio_in;
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g.rc_5.radio_max = g.rc_5.radio_in;
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g.rc_6.radio_max = g.rc_6.radio_in;
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g.rc_7.radio_max = g.rc_7.radio_in;
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g.rc_8.radio_max = g.rc_8.radio_in;
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g.rc_1.radio_trim = g.rc_1.radio_in;
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g.rc_2.radio_trim = g.rc_2.radio_in;
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g.rc_4.radio_trim = g.rc_4.radio_in;
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// 3 is not trimed
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g.rc_5.radio_trim = 1500;
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g.rc_6.radio_trim = 1500;
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g.rc_7.radio_trim = 1500;
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g.rc_8.radio_trim = 1500;
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Serial.printf_P(PSTR("\nMove all controls to each extreme. Hit Enter to save: "));
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while(1){
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delay(20);
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// Filters radio input - adjust filters in the radio.pde file
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// ----------------------------------------------------------
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read_radio();
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g.rc_1.update_min_max();
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g.rc_2.update_min_max();
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g.rc_3.update_min_max();
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g.rc_4.update_min_max();
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g.rc_5.update_min_max();
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g.rc_6.update_min_max();
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g.rc_7.update_min_max();
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g.rc_8.update_min_max();
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if(Serial.available() > 0){
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Serial.flush();
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save_EEPROM_radio();
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print_done();
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break;
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}
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}
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report_radio();
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return(0);
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}
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static int8_t
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setup_motors(uint8_t argc, const Menu::arg *argv)
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{
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report_frame();
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init_rc_in();
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// read the radio to set trims
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// ---------------------------
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trim_radio();
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print_hit_enter();
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delay(1000);
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int out_min = g.rc_3.radio_min + 70;
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while(1){
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delay(20);
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read_radio();
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motor_out[CH_1] = g.rc_3.radio_min;
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motor_out[CH_2] = g.rc_3.radio_min;
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motor_out[CH_3] = g.rc_3.radio_min;
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motor_out[CH_4] = g.rc_3.radio_min;
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if(g.frame_type == PLUS_FRAME){
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if(g.rc_1.control_in > 0){
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motor_out[CH_1] = out_min;
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Serial.println("0");
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}else if(g.rc_1.control_in < 0){
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motor_out[CH_2] = out_min;
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Serial.println("1");
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}
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if(g.rc_2.control_in > 0){
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motor_out[CH_4] = out_min;
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Serial.println("3");
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}else if(g.rc_2.control_in < 0){
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motor_out[CH_3] = out_min;
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Serial.println("2");
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}
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}else if(g.frame_type == X_FRAME){
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// lower right
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if((g.rc_1.control_in > 0) && (g.rc_2.control_in > 0)){
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motor_out[CH_4] = out_min;
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Serial.println("3");
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// lower left
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}else if((g.rc_1.control_in < 0) && (g.rc_2.control_in > 0)){
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motor_out[CH_2] = out_min;
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Serial.println("1");
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// upper left
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}else if((g.rc_1.control_in < 0) && (g.rc_2.control_in < 0)){
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motor_out[CH_3] = out_min;
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Serial.println("2");
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// upper right
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}else if((g.rc_1.control_in > 0) && (g.rc_2.control_in < 0)){
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motor_out[CH_1] = out_min;
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Serial.println("0");
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}
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}else if(g.frame_type == TRI_FRAME){
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if(g.rc_1.control_in > 0){
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motor_out[CH_1] = out_min;
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}else if(g.rc_1.control_in < 0){
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motor_out[CH_2] = out_min;
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}
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if(g.rc_2.control_in > 0){
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motor_out[CH_4] = out_min;
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}
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if(g.rc_4.control_in > 0){
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g.rc_4.servo_out = 2000;
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}else if(g.rc_4.control_in < 0){
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g.rc_4.servo_out = -2000;
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}
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g.rc_4.calc_pwm();
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motor_out[CH_3] = g.rc_4.radio_out;
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}
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if(g.rc_3.control_in > 0){
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APM_RC.OutputCh(CH_1, g.rc_3.radio_in);
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APM_RC.OutputCh(CH_2, g.rc_3.radio_in);
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APM_RC.OutputCh(CH_3, g.rc_3.radio_in);
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if(g.frame_type != TRI_FRAME)
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APM_RC.OutputCh(CH_4, g.rc_3.radio_in);
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}else{
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APM_RC.OutputCh(CH_1, motor_out[CH_1]);
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APM_RC.OutputCh(CH_2, motor_out[CH_2]);
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APM_RC.OutputCh(CH_3, motor_out[CH_3]);
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APM_RC.OutputCh(CH_4, motor_out[CH_4]);
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}
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if(Serial.available() > 0){
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return (0);
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}
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}
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}
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static int8_t
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setup_accel(uint8_t argc, const Menu::arg *argv)
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{
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Serial.printf_P(PSTR("\nHold ArduCopter completely still and level.\n"));
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imu.init_accel();
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print_accel_offsets();
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report_imu();
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return(0);
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}
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static int8_t
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setup_pid(uint8_t argc, const Menu::arg *argv)
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{
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if (!strcmp_P(argv[1].str, PSTR("default"))) {
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default_gains();
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}else if (!strcmp_P(argv[1].str, PSTR("s_kp"))) {
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g.pid_stabilize_roll.kP(argv[2].f);
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g.pid_stabilize_pitch.kP(argv[2].f);
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save_EEPROM_PID();
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}else if (!strcmp_P(argv[1].str, PSTR("s_kd"))) {
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g.stabilize_dampener = argv[2].f;
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save_EEPROM_PID();
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}else if (!strcmp_P(argv[1].str, PSTR("y_kp"))) {
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g.pid_yaw.kP(argv[2].f);
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save_EEPROM_PID();
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}else if (!strcmp_P(argv[1].str, PSTR("y_kd"))) {
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g.pid_yaw.kD(argv[2].f);
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save_EEPROM_PID();
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}else if (!strcmp_P(argv[1].str, PSTR("t_kp"))) {
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g.pid_baro_throttle.kP(argv[2].f);
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save_EEPROM_PID();
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}else if (!strcmp_P(argv[1].str, PSTR("t_kd"))) {
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g.pid_baro_throttle.kD(argv[2].f);
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save_EEPROM_PID();
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}else{
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default_gains();
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}
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report_gains();
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}
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static int8_t
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setup_flightmodes(uint8_t argc, const Menu::arg *argv)
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{
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byte switchPosition, oldSwitchPosition, mode;
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Serial.printf_P(PSTR("\nMove RC toggle switch to each position to edit, move aileron stick to select modes."));
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print_hit_enter();
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trim_radio();
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while(1){
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delay(20);
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read_radio();
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switchPosition = readSwitch();
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// look for control switch change
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if (oldSwitchPosition != switchPosition){
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mode = g.flight_modes[switchPosition];
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mode = constrain(mode, 0, NUM_MODES-1);
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// update the user
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print_switch(switchPosition, mode);
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// Remember switch position
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oldSwitchPosition = switchPosition;
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}
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// look for stick input
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if (radio_input_switch() == true){
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mode++;
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if(mode >= NUM_MODES)
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mode = 0;
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// save new mode
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g.flight_modes[switchPosition] = mode;
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// print new mode
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print_switch(switchPosition, mode);
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}
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// escape hatch
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if(Serial.available() > 0){
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g.flight_modes.save();
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print_done();
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report_flight_modes();
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return (0);
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}
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}
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}
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static int8_t
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setup_declination(uint8_t argc, const Menu::arg *argv)
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{
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compass.set_declination(radians(argv[1].f));
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report_compass();
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}
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static int8_t
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setup_erase(uint8_t argc, const Menu::arg *argv)
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{
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zero_eeprom();
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return 0;
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}
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static int8_t
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setup_compass(uint8_t argc, const Menu::arg *argv)
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{
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if (!strcmp_P(argv[1].str, PSTR("on"))) {
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g.compass_enabled = true;
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init_compass();
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} else if (!strcmp_P(argv[1].str, PSTR("off"))) {
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g.compass_enabled = false;
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}else{
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Serial.printf_P(PSTR("\nOptions:[on,off]\n"));
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report_compass();
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return 0;
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}
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g.compass_enabled.save();
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report_compass();
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return 0;
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}
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static int8_t
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setup_frame(uint8_t argc, const Menu::arg *argv)
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{
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if (!strcmp_P(argv[1].str, PSTR("+"))) {
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g.frame_type = PLUS_FRAME;
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} else if (!strcmp_P(argv[1].str, PSTR("x"))) {
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g.frame_type = X_FRAME;
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} else if (!strcmp_P(argv[1].str, PSTR("tri"))) {
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g.frame_type = TRI_FRAME;
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} else if (!strcmp_P(argv[1].str, PSTR("hexa"))) {
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g.frame_type = HEXA_FRAME;
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}else{
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Serial.printf_P(PSTR("\nOptions:[+, x, tri, hexa]\n"));
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report_frame();
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return 0;
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}
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g.frame_type.save();
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report_frame();
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return 0;
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}
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static int8_t
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setup_current(uint8_t argc, const Menu::arg *argv)
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{
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if (!strcmp_P(argv[1].str, PSTR("on"))) {
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g.current_enabled.set_and_save(true);
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} else if (!strcmp_P(argv[1].str, PSTR("off"))) {
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g.current_enabled.set_and_save(false);
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} else if(argv[1].i > 10){
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g.milliamp_hours.set_and_save(argv[1].i);
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}else{
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Serial.printf_P(PSTR("\nOptions:[on, off, mAh]\n"));
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report_current();
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return 0;
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}
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report_current();
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return 0;
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}
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static int8_t
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setup_sonar(uint8_t argc, const Menu::arg *argv)
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{
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if (!strcmp_P(argv[1].str, PSTR("on"))) {
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g.sonar_enabled.set_and_save(true);
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} else if (!strcmp_P(argv[1].str, PSTR("off"))) {
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g.sonar_enabled.set_and_save(false);
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}else{
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Serial.printf_P(PSTR("\nOptions:[on, off]\n"));
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report_sonar();
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return 0;
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}
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report_sonar();
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return 0;
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}
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/*static int8_t
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setup_mag_offset(uint8_t argc, const Menu::arg *argv)
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{
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Serial.printf_P(PSTR("\nRotate/Pitch/Roll your ArduCopter until the offset variables stop changing.\n"));
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print_hit_enter();
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Serial.printf_P(PSTR("Starting in 3 secs.\n"));
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delay(3000);
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compass.init(); // Initialization
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compass.set_orientation(MAG_ORIENTATION); // set compass's orientation on aircraft
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//compass.set_offsets(0, 0, 0); // set offsets to account for surrounding interference
|
|
//int counter = 0;
|
|
float _min[3], _max[3], _offset[3];
|
|
|
|
while(1){
|
|
static float min[3], _max[3], offset[3];
|
|
if (millis() - fast_loopTimer > 100) {
|
|
delta_ms_fast_loop = millis() - fast_loopTimer;
|
|
fast_loopTimer = millis();
|
|
G_Dt = (float)delta_ms_fast_loop / 1000.f;
|
|
|
|
|
|
compass.read();
|
|
compass.calculate(0, 0); // roll = 0, pitch = 0 for this example
|
|
|
|
// capture min
|
|
if(compass.mag_x < _min[0]) _min[0] = compass.mag_x;
|
|
if(compass.mag_y < _min[1]) _min[1] = compass.mag_y;
|
|
if(compass.mag_z < _min[2]) _min[2] = compass.mag_z;
|
|
|
|
// capture max
|
|
if(compass.mag_x > _max[0]) _max[0] = compass.mag_x;
|
|
if(compass.mag_y > _max[1]) _max[1] = compass.mag_y;
|
|
if(compass.mag_z > _max[2]) _max[2] = compass.mag_z;
|
|
|
|
// calculate offsets
|
|
offset[0] = -(_max[0] + _min[0]) / 2;
|
|
offset[1] = -(_max[1] + _min[1]) / 2;
|
|
offset[2] = -(_max[2] + _min[2]) / 2;
|
|
|
|
// display all to user
|
|
Serial.printf_P(PSTR("Heading: "));
|
|
Serial.print(ToDeg(compass.heading));
|
|
Serial.print(" \t(");
|
|
Serial.print(compass.mag_x);
|
|
Serial.print(",");
|
|
Serial.print(compass.mag_y);
|
|
Serial.print(",");
|
|
Serial.print(compass.mag_z);
|
|
Serial.print(")\t offsets(");
|
|
Serial.print(offset[0]);
|
|
Serial.print(",");
|
|
Serial.print(offset[1]);
|
|
Serial.print(",");
|
|
Serial.print(offset[2]);
|
|
Serial.println(")");
|
|
|
|
if(Serial.available() > 0){
|
|
|
|
|
|
//mag_offset_x = offset[0];
|
|
//mag_offset_y = offset[1];
|
|
//mag_offset_z = offset[2];
|
|
|
|
//setup_mag_offset();
|
|
|
|
// set offsets to account for surrounding interference
|
|
//compass.set_offsets(mag_offset_x, mag_offset_y, mag_offset_z);
|
|
|
|
report_compass();
|
|
break;
|
|
}
|
|
}
|
|
}
|
|
}
|
|
*/
|
|
|
|
|
|
/***************************************************************************/
|
|
// CLI defaults
|
|
/***************************************************************************/
|
|
|
|
void default_waypoint_info()
|
|
{
|
|
g.waypoint_radius = 4; //TODO: Replace this quick fix with a real way to define wp_radius
|
|
g.loiter_radius = 30; //TODO: Replace this quick fix with a real way to define loiter_radius
|
|
save_EEPROM_waypoint_info();
|
|
}
|
|
|
|
|
|
void
|
|
default_nav()
|
|
{
|
|
// nav control
|
|
g.crosstrack_gain = XTRACK_GAIN * 100;
|
|
g.crosstrack_entry_angle = XTRACK_ENTRY_ANGLE * 100;
|
|
g.pitch_max = PITCH_MAX * 100;
|
|
save_EEPROM_nav();
|
|
}
|
|
|
|
void
|
|
default_alt_hold()
|
|
{
|
|
g.RTL_altitude.set_and_save(-1);
|
|
}
|
|
|
|
void
|
|
default_frame()
|
|
{
|
|
g.frame_type.set_and_save(PLUS_FRAME);
|
|
}
|
|
|
|
void
|
|
default_current()
|
|
{
|
|
g.milliamp_hours = 2000;
|
|
g.current_enabled.set(false);
|
|
save_EEPROM_current();
|
|
}
|
|
|
|
void
|
|
default_flight_modes()
|
|
{
|
|
g.flight_modes[0] = FLIGHT_MODE_1;
|
|
g.flight_modes[1] = FLIGHT_MODE_2;
|
|
g.flight_modes[2] = FLIGHT_MODE_3;
|
|
g.flight_modes[3] = FLIGHT_MODE_4;
|
|
g.flight_modes[4] = FLIGHT_MODE_5;
|
|
g.flight_modes[5] = FLIGHT_MODE_6;
|
|
g.flight_modes.save();
|
|
}
|
|
|
|
void
|
|
default_throttle()
|
|
{
|
|
g.throttle_min = THROTTLE_MIN;
|
|
g.throttle_max = THROTTLE_MAX;
|
|
g.throttle_cruise = THROTTLE_CRUISE;
|
|
g.throttle_fs_enabled = THROTTLE_FAILSAFE;
|
|
g.throttle_fs_action = THROTTLE_FAILSAFE_ACTION;
|
|
g.throttle_fs_value = THROTTLE_FS_VALUE;
|
|
save_EEPROM_throttle();
|
|
}
|
|
|
|
void default_log_bitmask()
|
|
{
|
|
|
|
// convenience macro for testing LOG_* and setting LOGBIT_*
|
|
#define LOGBIT(_s) (MASK_LOG_##_s ? MASK_LOG_##_s : 0)
|
|
|
|
g.log_bitmask =
|
|
LOGBIT(ATTITUDE_FAST) |
|
|
LOGBIT(ATTITUDE_MED) |
|
|
LOGBIT(GPS) |
|
|
LOGBIT(PM) |
|
|
LOGBIT(CTUN) |
|
|
LOGBIT(NTUN) |
|
|
LOGBIT(MODE) |
|
|
LOGBIT(RAW) |
|
|
LOGBIT(CMD) |
|
|
LOGBIT(CUR);
|
|
#undef LOGBIT
|
|
|
|
g.log_bitmask.save();
|
|
}
|
|
|
|
|
|
void
|
|
default_gains()
|
|
{
|
|
// acro, angular rate
|
|
g.pid_acro_rate_roll.kP(ACRO_RATE_ROLL_P);
|
|
g.pid_acro_rate_roll.kI(ACRO_RATE_ROLL_I);
|
|
g.pid_acro_rate_roll.kD(0);
|
|
g.pid_acro_rate_roll.imax(ACRO_RATE_ROLL_IMAX * 100);
|
|
|
|
g.pid_acro_rate_pitch.kP(ACRO_RATE_PITCH_P);
|
|
g.pid_acro_rate_pitch.kI(ACRO_RATE_PITCH_I);
|
|
g.pid_acro_rate_pitch.kD(0);
|
|
g.pid_acro_rate_pitch.imax(ACRO_RATE_PITCH_IMAX * 100);
|
|
|
|
g.pid_acro_rate_yaw.kP(ACRO_RATE_YAW_P);
|
|
g.pid_acro_rate_yaw.kI(ACRO_RATE_YAW_I);
|
|
g.pid_acro_rate_yaw.kD(0);
|
|
g.pid_acro_rate_yaw.imax(ACRO_RATE_YAW_IMAX * 100);
|
|
|
|
|
|
// stabilize, angle error
|
|
g.pid_stabilize_roll.kP(STABILIZE_ROLL_P);
|
|
g.pid_stabilize_roll.kI(STABILIZE_ROLL_I);
|
|
g.pid_stabilize_roll.kD(0);
|
|
g.pid_stabilize_roll.imax(STABILIZE_ROLL_IMAX * 100);
|
|
|
|
g.pid_stabilize_pitch.kP(STABILIZE_PITCH_P);
|
|
g.pid_stabilize_pitch.kI(STABILIZE_PITCH_I);
|
|
g.pid_stabilize_pitch.kD(0);
|
|
g.pid_stabilize_pitch.imax(STABILIZE_PITCH_IMAX * 100);
|
|
|
|
// YAW hold
|
|
g.pid_yaw.kP(YAW_P);
|
|
g.pid_yaw.kI(YAW_I);
|
|
g.pid_yaw.kD(0);
|
|
g.pid_yaw.imax(YAW_IMAX * 100);
|
|
|
|
|
|
// custom dampeners
|
|
// roll pitch
|
|
g.stabilize_dampener = STABILIZE_DAMPENER;
|
|
|
|
//yaw
|
|
g.hold_yaw_dampener = HOLD_YAW_DAMPENER;
|
|
|
|
// navigation
|
|
g.pid_nav_lat.kP(NAV_P);
|
|
g.pid_nav_lat.kI(NAV_I);
|
|
g.pid_nav_lat.kD(NAV_D);
|
|
g.pid_nav_lat.imax(NAV_IMAX);
|
|
|
|
g.pid_nav_lon.kP(NAV_P);
|
|
g.pid_nav_lon.kI(NAV_I);
|
|
g.pid_nav_lon.kD(NAV_D);
|
|
g.pid_nav_lon.imax(NAV_IMAX);
|
|
|
|
g.pid_baro_throttle.kP(THROTTLE_BARO_P);
|
|
g.pid_baro_throttle.kI(THROTTLE_BARO_I);
|
|
g.pid_baro_throttle.kD(THROTTLE_BARO_D);
|
|
g.pid_baro_throttle.imax(THROTTLE_BARO_IMAX);
|
|
|
|
g.pid_sonar_throttle.kP(THROTTLE_SONAR_P);
|
|
g.pid_sonar_throttle.kI(THROTTLE_SONAR_I);
|
|
g.pid_sonar_throttle.kD(THROTTLE_SONAR_D);
|
|
g.pid_sonar_throttle.imax(THROTTLE_SONAR_IMAX);
|
|
|
|
save_EEPROM_PID();
|
|
}
|
|
|
|
|
|
|
|
/***************************************************************************/
|
|
// CLI reports
|
|
/***************************************************************************/
|
|
|
|
void report_current()
|
|
{
|
|
read_EEPROM_current();
|
|
Serial.printf_P(PSTR("Current Sensor\n"));
|
|
print_divider();
|
|
print_enabled(g.current_enabled.get());
|
|
|
|
Serial.printf_P(PSTR("mah: %d"),(int)g.milliamp_hours.get());
|
|
print_blanks(2);
|
|
}
|
|
|
|
void report_sonar()
|
|
{
|
|
g.sonar_enabled.load();
|
|
Serial.printf_P(PSTR("Sonar Sensor\n"));
|
|
print_divider();
|
|
print_enabled(g.sonar_enabled.get());
|
|
print_blanks(2);
|
|
}
|
|
|
|
|
|
void report_frame()
|
|
{
|
|
Serial.printf_P(PSTR("Frame\n"));
|
|
print_divider();
|
|
|
|
|
|
if(g.frame_type == X_FRAME)
|
|
Serial.printf_P(PSTR("X "));
|
|
else if(g.frame_type == PLUS_FRAME)
|
|
Serial.printf_P(PSTR("Plus "));
|
|
else if(g.frame_type == TRI_FRAME)
|
|
Serial.printf_P(PSTR("TRI "));
|
|
else if(g.frame_type == HEXA_FRAME)
|
|
Serial.printf_P(PSTR("HEXA "));
|
|
|
|
Serial.printf_P(PSTR("frame (%d)"), (int)g.frame_type);
|
|
print_blanks(2);
|
|
}
|
|
|
|
void report_radio()
|
|
{
|
|
Serial.printf_P(PSTR("Radio\n"));
|
|
print_divider();
|
|
// radio
|
|
read_EEPROM_radio();
|
|
print_radio_values();
|
|
print_blanks(2);
|
|
}
|
|
|
|
void report_gains()
|
|
{
|
|
Serial.printf_P(PSTR("Gains\n"));
|
|
print_divider();
|
|
|
|
read_EEPROM_PID();
|
|
// Acro
|
|
Serial.printf_P(PSTR("Acro:\nroll:\n"));
|
|
print_PID(&g.pid_acro_rate_roll);
|
|
Serial.printf_P(PSTR("pitch:\n"));
|
|
print_PID(&g.pid_acro_rate_pitch);
|
|
Serial.printf_P(PSTR("yaw:\n"));
|
|
print_PID(&g.pid_acro_rate_yaw);
|
|
|
|
// Stabilize
|
|
Serial.printf_P(PSTR("\nStabilize:\nroll:\n"));
|
|
print_PID(&g.pid_stabilize_roll);
|
|
Serial.printf_P(PSTR("pitch:\n"));
|
|
print_PID(&g.pid_stabilize_pitch);
|
|
Serial.printf_P(PSTR("yaw:\n"));
|
|
print_PID(&g.pid_yaw);
|
|
|
|
Serial.printf_P(PSTR("Stabilize dampener: %4.3f\n"), (float)g.stabilize_dampener);
|
|
Serial.printf_P(PSTR("Yaw Dampener: %4.3f\n\n"), (float)g.hold_yaw_dampener);
|
|
|
|
// Nav
|
|
Serial.printf_P(PSTR("Nav:\nlat:\n"));
|
|
print_PID(&g.pid_nav_lat);
|
|
Serial.printf_P(PSTR("long:\n"));
|
|
print_PID(&g.pid_nav_lon);
|
|
Serial.printf_P(PSTR("baro throttle:\n"));
|
|
print_PID(&g.pid_baro_throttle);
|
|
Serial.printf_P(PSTR("sonar throttle:\n"));
|
|
print_PID(&g.pid_sonar_throttle);
|
|
print_blanks(2);
|
|
}
|
|
|
|
void report_xtrack()
|
|
{
|
|
Serial.printf_P(PSTR("Crosstrack\n"));
|
|
print_divider();
|
|
// radio
|
|
read_EEPROM_nav();
|
|
Serial.printf_P(PSTR("XTRACK: %4.2f\n"
|
|
"XTRACK angle: %d\n"
|
|
"PITCH_MAX: %ld"),
|
|
(float)g.crosstrack_gain,
|
|
(int)g.crosstrack_entry_angle,
|
|
(long)g.pitch_max);
|
|
print_blanks(2);
|
|
}
|
|
|
|
void report_throttle()
|
|
{
|
|
Serial.printf_P(PSTR("Throttle\n"));
|
|
print_divider();
|
|
|
|
read_EEPROM_throttle();
|
|
Serial.printf_P(PSTR("min: %d\n"
|
|
"max: %d\n"
|
|
"cruise: %d\n"
|
|
"failsafe_enabled: %d\n"
|
|
"failsafe_value: %d"),
|
|
(int)g.throttle_min,
|
|
(int)g.throttle_max,
|
|
(int)g.throttle_cruise,
|
|
(int)g.throttle_fs_enabled,
|
|
(int)g.throttle_fs_value);
|
|
print_blanks(2);
|
|
}
|
|
|
|
void report_imu()
|
|
{
|
|
Serial.printf_P(PSTR("IMU\n"));
|
|
print_divider();
|
|
|
|
print_gyro_offsets();
|
|
print_accel_offsets();
|
|
print_blanks(2);
|
|
}
|
|
|
|
void report_compass()
|
|
{
|
|
Serial.printf_P(PSTR("Compass\n"));
|
|
print_divider();
|
|
|
|
print_enabled(g.compass_enabled);
|
|
|
|
// mag declination
|
|
Serial.printf_P(PSTR("Mag Delination: %4.4f\n"),
|
|
degrees(compass.get_declination()));
|
|
|
|
Vector3f offsets = compass.get_offsets();
|
|
|
|
// mag offsets
|
|
Serial.printf_P(PSTR("Mag offsets: %4.4f, %4.4f, %4.4f"),
|
|
offsets.x,
|
|
offsets.y,
|
|
offsets.z);
|
|
print_blanks(2);
|
|
}
|
|
|
|
void report_flight_modes()
|
|
{
|
|
Serial.printf_P(PSTR("Flight modes\n"));
|
|
print_divider();
|
|
|
|
for(int i = 0; i < 6; i++ ){
|
|
print_switch(i, g.flight_modes[i]);
|
|
}
|
|
print_blanks(2);
|
|
}
|
|
|
|
/***************************************************************************/
|
|
// CLI utilities
|
|
/***************************************************************************/
|
|
|
|
void
|
|
print_PID(PID * pid)
|
|
{
|
|
Serial.printf_P(PSTR("P: %4.3f, I:%4.3f, D:%4.3f, IMAX:%ld\n"), pid->kP(), pid->kI(), pid->kD(), (long)pid->imax());
|
|
}
|
|
|
|
void
|
|
print_radio_values()
|
|
{
|
|
Serial.printf_P(PSTR("CH1: %d | %d\n"), (int)g.rc_1.radio_min, (int)g.rc_1.radio_max);
|
|
Serial.printf_P(PSTR("CH2: %d | %d\n"), (int)g.rc_2.radio_min, (int)g.rc_2.radio_max);
|
|
Serial.printf_P(PSTR("CH3: %d | %d\n"), (int)g.rc_3.radio_min, (int)g.rc_3.radio_max);
|
|
Serial.printf_P(PSTR("CH4: %d | %d\n"), (int)g.rc_4.radio_min, (int)g.rc_4.radio_max);
|
|
Serial.printf_P(PSTR("CH5: %d | %d\n"), (int)g.rc_5.radio_min, (int)g.rc_5.radio_max);
|
|
Serial.printf_P(PSTR("CH6: %d | %d\n"), (int)g.rc_6.radio_min, (int)g.rc_6.radio_max);
|
|
Serial.printf_P(PSTR("CH7: %d | %d\n"), (int)g.rc_7.radio_min, (int)g.rc_7.radio_max);
|
|
Serial.printf_P(PSTR("CH8: %d | %d\n"), (int)g.rc_8.radio_min, (int)g.rc_8.radio_max);
|
|
}
|
|
|
|
void
|
|
print_switch(byte p, byte m)
|
|
{
|
|
Serial.printf_P(PSTR("Pos %d: "),p);
|
|
Serial.println(flight_mode_strings[m]);
|
|
}
|
|
|
|
void
|
|
print_done()
|
|
{
|
|
Serial.printf_P(PSTR("\nSaved Settings\n\n"));
|
|
}
|
|
|
|
void
|
|
print_blanks(int num)
|
|
{
|
|
while(num > 0){
|
|
num--;
|
|
Serial.println("");
|
|
}
|
|
}
|
|
|
|
void
|
|
print_divider(void)
|
|
{
|
|
for (int i = 0; i < 40; i++) {
|
|
Serial.print("-");
|
|
}
|
|
Serial.println("");
|
|
}
|
|
|
|
int8_t
|
|
radio_input_switch(void)
|
|
{
|
|
static int8_t bouncer = 0;
|
|
|
|
if (int16_t(g.rc_1.radio_in - g.rc_1.radio_trim) > 100) {
|
|
bouncer = 10;
|
|
}
|
|
if (int16_t(g.rc_1.radio_in - g.rc_1.radio_trim) < -100) {
|
|
bouncer = -10;
|
|
}
|
|
if (bouncer >0) {
|
|
bouncer --;
|
|
}
|
|
if (bouncer <0) {
|
|
bouncer ++;
|
|
}
|
|
|
|
if (bouncer == 1 || bouncer == -1) {
|
|
return bouncer;
|
|
}else{
|
|
return 0;
|
|
}
|
|
}
|
|
|
|
|
|
void zero_eeprom(void)
|
|
{
|
|
byte b;
|
|
Serial.printf_P(PSTR("\nErasing EEPROM\n"));
|
|
for (int i = 0; i < EEPROM_MAX_ADDR; i++) {
|
|
eeprom_write_byte((uint8_t *) i, b);
|
|
}
|
|
Serial.printf_P(PSTR("done\n"));
|
|
}
|
|
|
|
void print_enabled(boolean b)
|
|
{
|
|
if(b)
|
|
Serial.printf_P(PSTR("en"));
|
|
else
|
|
Serial.printf_P(PSTR("dis"));
|
|
Serial.printf_P(PSTR("abled\n"));
|
|
}
|
|
|
|
void
|
|
print_accel_offsets(void)
|
|
{
|
|
Serial.printf_P(PSTR("Accel offsets: %4.2f, %4.2f, %4.2f\n"),
|
|
(float)imu.ax(),
|
|
(float)imu.ay(),
|
|
(float)imu.az());
|
|
}
|
|
|
|
void
|
|
print_gyro_offsets(void)
|
|
{
|
|
Serial.printf_P(PSTR("Gyro offsets: %4.2f, %4.2f, %4.2f\n"),
|
|
(float)imu.gx(),
|
|
(float)imu.gy(),
|
|
(float)imu.gz());
|
|
}
|
|
|
|
|
|
|
|
/***************************************************************************/
|
|
// EEPROM convenience functions
|
|
/***************************************************************************/
|
|
|
|
|
|
void read_EEPROM_waypoint_info(void)
|
|
{
|
|
g.waypoint_total.load();
|
|
g.waypoint_radius.load();
|
|
g.loiter_radius.load();
|
|
}
|
|
|
|
void save_EEPROM_waypoint_info(void)
|
|
{
|
|
g.waypoint_total.save();
|
|
g.waypoint_radius.save();
|
|
g.loiter_radius.save();
|
|
}
|
|
|
|
/********************************************************************************/
|
|
|
|
void read_EEPROM_nav(void)
|
|
{
|
|
g.crosstrack_gain.load();
|
|
g.crosstrack_entry_angle.load();
|
|
g.pitch_max.load();
|
|
}
|
|
|
|
void save_EEPROM_nav(void)
|
|
{
|
|
g.crosstrack_gain.save();
|
|
g.crosstrack_entry_angle.save();
|
|
g.pitch_max.save();
|
|
}
|
|
|
|
/********************************************************************************/
|
|
|
|
void read_EEPROM_PID(void)
|
|
{
|
|
g.pid_acro_rate_roll.load_gains();
|
|
g.pid_acro_rate_pitch.load_gains();
|
|
g.pid_acro_rate_yaw.load_gains();
|
|
|
|
g.pid_stabilize_roll.load_gains();
|
|
g.pid_stabilize_pitch.load_gains();
|
|
g.pid_yaw.load_gains();
|
|
|
|
g.pid_nav_lon.load_gains();
|
|
g.pid_nav_lat.load_gains();
|
|
g.pid_baro_throttle.load_gains();
|
|
g.pid_sonar_throttle.load_gains();
|
|
|
|
// roll pitch
|
|
g.stabilize_dampener.load();
|
|
|
|
// yaw
|
|
g.hold_yaw_dampener.load();
|
|
init_pids();
|
|
}
|
|
|
|
void save_EEPROM_PID(void)
|
|
{
|
|
|
|
g.pid_acro_rate_roll.save_gains();
|
|
g.pid_acro_rate_pitch.save_gains();
|
|
g.pid_acro_rate_yaw.save_gains();
|
|
|
|
g.pid_stabilize_roll.save_gains();
|
|
g.pid_stabilize_pitch.save_gains();
|
|
g.pid_yaw.save_gains();
|
|
|
|
g.pid_nav_lon.save_gains();
|
|
g.pid_nav_lat.save_gains();
|
|
g.pid_baro_throttle.save_gains();
|
|
g.pid_sonar_throttle.save_gains();
|
|
|
|
// roll pitch
|
|
g.stabilize_dampener.save();
|
|
// yaw
|
|
g.hold_yaw_dampener.save();
|
|
}
|
|
|
|
/********************************************************************************/
|
|
|
|
void save_EEPROM_current(void)
|
|
{
|
|
g.current_enabled.save();
|
|
g.milliamp_hours.save();
|
|
}
|
|
|
|
void read_EEPROM_current(void)
|
|
{
|
|
g.current_enabled.load();
|
|
g.milliamp_hours.load();
|
|
}
|
|
|
|
/********************************************************************************/
|
|
|
|
void read_EEPROM_radio(void)
|
|
{
|
|
g.rc_1.load_eeprom();
|
|
g.rc_2.load_eeprom();
|
|
g.rc_3.load_eeprom();
|
|
g.rc_4.load_eeprom();
|
|
g.rc_5.load_eeprom();
|
|
g.rc_6.load_eeprom();
|
|
g.rc_7.load_eeprom();
|
|
g.rc_8.load_eeprom();
|
|
}
|
|
|
|
void save_EEPROM_radio(void)
|
|
{
|
|
g.rc_1.save_eeprom();
|
|
g.rc_2.save_eeprom();
|
|
g.rc_3.save_eeprom();
|
|
g.rc_4.save_eeprom();
|
|
g.rc_5.save_eeprom();
|
|
g.rc_6.save_eeprom();
|
|
g.rc_7.save_eeprom();
|
|
g.rc_8.save_eeprom();
|
|
}
|
|
|
|
/********************************************************************************/
|
|
// configs are the basics
|
|
void read_EEPROM_throttle(void)
|
|
{
|
|
g.throttle_min.load();
|
|
g.throttle_max.load();
|
|
g.throttle_cruise.load();
|
|
g.throttle_fs_enabled.load();
|
|
g.throttle_fs_action.load();
|
|
g.throttle_fs_value.load();
|
|
}
|
|
|
|
void save_EEPROM_throttle(void)
|
|
{
|
|
g.throttle_min.load();
|
|
g.throttle_max.load();
|
|
g.throttle_cruise.save();
|
|
g.throttle_fs_enabled.load();
|
|
g.throttle_fs_action.load();
|
|
g.throttle_fs_value.load();
|
|
}
|
|
|
|
|
|
/********************************************************************************/
|
|
/*
|
|
float
|
|
read_EE_float(int address)
|
|
{
|
|
union {
|
|
byte bytes[4];
|
|
float value;
|
|
} _floatOut;
|
|
|
|
for (int i = 0; i < 4; i++)
|
|
_floatOut.bytes[i] = eeprom_read_byte((uint8_t *) (address + i));
|
|
return _floatOut.value;
|
|
}
|
|
|
|
void write_EE_float(float value, int address)
|
|
{
|
|
union {
|
|
byte bytes[4];
|
|
float value;
|
|
} _floatIn;
|
|
|
|
_floatIn.value = value;
|
|
for (int i = 0; i < 4; i++)
|
|
eeprom_write_byte((uint8_t *) (address + i), _floatIn.bytes[i]);
|
|
}
|
|
*/
|
|
/********************************************************************************/
|
|
/*
|
|
float
|
|
read_EE_compressed_float(int address, byte places)
|
|
{
|
|
float scale = pow(10, places);
|
|
|
|
int temp = eeprom_read_word((uint16_t *) address);
|
|
return ((float)temp / scale);
|
|
}
|
|
|
|
void write_EE_compressed_float(float value, int address, byte places)
|
|
{
|
|
float scale = pow(10, places);
|
|
int temp = value * scale;
|
|
eeprom_write_word((uint16_t *) address, temp);
|
|
}
|
|
*/ |