mirror of https://github.com/ArduPilot/ardupilot
718 lines
18 KiB
Plaintext
718 lines
18 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_esc (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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static int8_t setup_accel (uint8_t argc, const Menu::arg *argv);
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static int8_t setup_accel_flat (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_declination (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_compass_enable (uint8_t argc, const Menu::arg *argv);
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static int8_t setup_compass_disable (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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{"reset", setup_factory},
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{"erase", setup_erase},
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{"radio", setup_radio},
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{"esc", setup_esc},
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{"level", setup_accel},
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{"flat", setup_accel_flat},
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{"modes", setup_flightmodes},
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{"pid", setup_pid},
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{"frame", setup_frame},
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{"enable_mag", setup_compass_enable},
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{"disable_mag", setup_compass_disable},
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{"compass", setup_compass},
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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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Serial.printf_P(PSTR("\nRadio:\n"));
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// radio
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read_EEPROM_radio();
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print_radio_values();
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// frame
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read_EEPROM_frame();
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Serial.printf_P(PSTR("\nFrame type:"));
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Serial.printf_P(PSTR("%d \n"), (int)frame_type);
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if(frame_type == X_FRAME)
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Serial.printf_P(PSTR(" X\n"));
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else if(frame_type == PLUS_FRAME)
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Serial.printf_P(PSTR("Plus\n"));
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read_EEPROM_PID();
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Serial.printf_P(PSTR("\nGains:\n"));
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// Acro
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Serial.printf_P(PSTR("Acro:\nroll:\n"));
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print_PID(&pid_acro_rate_roll);
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Serial.printf_P(PSTR("pitch:\n"));
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print_PID(&pid_acro_rate_pitch);
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Serial.printf_P(PSTR("yaw:\n"));
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print_PID(&pid_acro_rate_yaw);
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Serial.printf_P(PSTR("rates:\n"));
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Serial.println(acro_rate_roll_pitch,3);
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Serial.printf_P(PSTR("rates_yaw:\n"));
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Serial.println(acro_rate_yaw,3);
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Serial.println(" ");
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// Stabilize
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Serial.printf_P(PSTR("Stabilize:\nroll:\n"));
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print_PID(&pid_stabilize_roll);
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Serial.printf_P(PSTR("pitch:\n"));
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print_PID(&pid_stabilize_pitch);
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Serial.printf_P(PSTR("yaw:\n"));
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print_PID(&pid_yaw);
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Serial.printf_P(PSTR("Rate stabilize:\n"));
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Serial.println(stabilize_rate_roll_pitch,3);
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Serial.println(" ");
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// Nav
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Serial.printf_P(PSTR("Nav:\npitch:\n"));
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print_PID(&pid_nav);
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Serial.printf_P(PSTR("throttle:\n"));
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print_PID(&pid_throttle);
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Serial.println(" ");
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// Crosstrack
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read_EEPROM_nav();
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Serial.printf_P(PSTR("XTRACK:"));
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Serial.println(x_track_gain,DEC);
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Serial.printf_P(PSTR("XTRACK angle: %d\n"), x_track_angle);
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Serial.printf_P(PSTR("PITCH_MAX: %d\n\n"), pitch_max);
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// User Configs
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read_EEPROM_configs();
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Serial.printf_P(PSTR("\nUser config:\n"));
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Serial.printf_P(PSTR("throttle_min: %d\n"), throttle_min);
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Serial.printf_P(PSTR("throttle_max: %d\n"), throttle_max);
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Serial.printf_P(PSTR("throttle_cruise: %d\n"), throttle_cruise);
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Serial.printf_P(PSTR("throttle_failsafe_enabled: %d\n"), throttle_failsafe_enabled);
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Serial.printf_P(PSTR("throttle_failsafe_value: %d\n"), throttle_failsafe_value);
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Serial.printf_P(PSTR("log_bitmask: %d\n\n"), log_bitmask);
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imu.print_gyro_offsets();
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imu.print_accel_offsets();
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// mag declination
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Serial.printf_P(PSTR("\nCompass "));
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if(compass_enabled)
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Serial.printf_P(PSTR("en"));
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else
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Serial.printf_P(PSTR("dis"));
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Serial.printf_P(PSTR("abled\n\n"));
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// mag declination
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read_EEPROM_mag_declination();
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Serial.printf_P(PSTR("Mag Delination: "));
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Serial.println(mag_declination,2);
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// mag offsets
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Serial.printf_P(PSTR("Mag offsets: "));
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Serial.print(mag_offset_x, 2);
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Serial.printf_P(PSTR(", "));
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Serial.print(mag_offset_y, 2);
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Serial.printf_P(PSTR(", "));
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Serial.println(mag_offset_z, 2);
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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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/*
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saves:
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save_EEPROM_waypoint_info();
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save_EEPROM_nav();
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save_EEPROM_flight_modes();
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save_EEPROM_configs();
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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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//Serial.printf_P(PSTR("\nFACTORY RESET\n\n"));
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//zero_eeprom();
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setup_pid(0 ,NULL);
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wp_radius = 4; //TODO: Replace this quick fix with a real way to define wp_radius
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loiter_radius = 30; //TODO: Replace this quick fix with a real way to define loiter_radius
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save_EEPROM_waypoint_info();
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// nav control
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x_track_gain = XTRACK_GAIN * 100;
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x_track_angle = XTRACK_ENTRY_ANGLE * 100;
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pitch_max = PITCH_MAX * 100;
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save_EEPROM_nav();
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// alt hold
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alt_to_hold = -1;
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save_EEPROM_alt_RTL();
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// default to a + configuration
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frame_type = PLUS_FRAME;
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save_EEPROM_frame();
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flight_modes[0] = FLIGHT_MODE_1;
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flight_modes[1] = FLIGHT_MODE_2;
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flight_modes[2] = FLIGHT_MODE_3;
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flight_modes[3] = FLIGHT_MODE_4;
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flight_modes[4] = FLIGHT_MODE_5;
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flight_modes[5] = FLIGHT_MODE_6;
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save_EEPROM_flight_modes();
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// user configs
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throttle_min = THROTTLE_MIN;
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throttle_max = THROTTLE_MAX;
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throttle_cruise = THROTTLE_CRUISE;
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throttle_failsafe_enabled = THROTTLE_FAILSAFE;
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throttle_failsafe_action = THROTTLE_FAILSAFE_ACTION;
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throttle_failsafe_value = THROTTLE_FS_VALUE;
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// convenience macro for testing LOG_* and setting LOGBIT_*
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#define LOGBIT(_s) (LOG_ ## _s ? LOGBIT_ ## _s : 0)
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log_bitmask =
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LOGBIT(ATTITUDE_FAST) |
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LOGBIT(ATTITUDE_MED) |
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LOGBIT(GPS) |
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LOGBIT(PM) |
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LOGBIT(CTUN) |
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LOGBIT(NTUN) |
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LOGBIT(MODE) |
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LOGBIT(RAW) |
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LOGBIT(CMD);
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#undef LOGBIT
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save_EEPROM_configs();
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print_done();
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// finish
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// ------
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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(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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rc_1.radio_min = rc_1.radio_in;
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rc_2.radio_min = rc_2.radio_in;
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rc_3.radio_min = rc_3.radio_in;
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rc_4.radio_min = rc_4.radio_in;
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rc_5.radio_min = rc_5.radio_in;
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rc_6.radio_min = rc_6.radio_in;
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rc_7.radio_min = rc_7.radio_in;
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rc_8.radio_min = rc_8.radio_in;
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rc_1.radio_max = rc_1.radio_in;
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rc_2.radio_max = rc_2.radio_in;
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rc_3.radio_max = rc_3.radio_in;
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rc_4.radio_max = rc_4.radio_in;
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rc_5.radio_max = rc_5.radio_in;
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rc_6.radio_max = rc_6.radio_in;
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rc_7.radio_max = rc_7.radio_in;
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rc_8.radio_max = rc_8.radio_in;
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rc_1.radio_trim = rc_1.radio_in;
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rc_2.radio_trim = rc_2.radio_in;
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rc_4.radio_trim = rc_4.radio_in;
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// 3 is not trimed
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rc_5.radio_trim = 1500;
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rc_6.radio_trim = 1500;
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rc_7.radio_trim = 1500;
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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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rc_1.update_min_max();
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rc_2.update_min_max();
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rc_3.update_min_max();
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rc_4.update_min_max();
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rc_5.update_min_max();
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rc_6.update_min_max();
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rc_7.update_min_max();
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rc_8.update_min_max();
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if(Serial.available() > 0){
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//rc_3.radio_max += 250;
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Serial.flush();
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save_EEPROM_radio();
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//delay(100);
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// double checking
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//read_EEPROM_radio();
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//print_radio_values();
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print_done();
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break;
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}
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}
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return(0);
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}
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static int8_t
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setup_esc(uint8_t argc, const Menu::arg *argv)
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{
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Serial.println("\n\nESC Setup - Motors armed");
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rc_3.load_eeprom();
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rc_1.set_filter(false);
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rc_2.set_filter(false);
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rc_3.set_filter(false);
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rc_4.set_filter(false);
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motor_armed = true;
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while(1){
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delay(20);
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read_radio();
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APM_RC.OutputCh(CH_1, rc_3.radio_in);
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APM_RC.OutputCh(CH_2, rc_3.radio_in);
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APM_RC.OutputCh(CH_3, rc_3.radio_in);
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APM_RC.OutputCh(CH_4, rc_3.radio_in);
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if(Serial.available() > 0){
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motor_armed = false;
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rc_1.set_filter(true);
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rc_2.set_filter(true);
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rc_3.set_filter(true);
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rc_4.set_filter(true);
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read_radio();
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Serial.println("\n\nMotors disarmed)");
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break;
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}
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}
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return(0);
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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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/*
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imu.init_gyro();
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print_gyro();
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imu.load_gyro_eeprom();
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print_gyro();
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*/
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imu.init_accel();
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imu.print_accel_offsets();
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//imu.load_accel_eeprom();
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//print_accel();
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return(0);
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}
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static int8_t
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setup_accel_flat(uint8_t argc, const Menu::arg *argv)
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{
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Serial.printf_P(PSTR("\nClear Accel offsets.\n"));
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imu.zero_accel();
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imu.print_accel_offsets();
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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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Serial.printf_P(PSTR("\nSetting default PID gains\n"));
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// acro, angular rate
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pid_acro_rate_roll.kP(ACRO_RATE_ROLL_P);
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pid_acro_rate_roll.kI(ACRO_RATE_ROLL_I);
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pid_acro_rate_roll.kD(ACRO_RATE_ROLL_D);
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pid_acro_rate_roll.imax(ACRO_RATE_ROLL_IMAX * 100);
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pid_acro_rate_pitch.kP(ACRO_RATE_PITCH_P);
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pid_acro_rate_pitch.kI(ACRO_RATE_PITCH_I);
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pid_acro_rate_pitch.kD(ACRO_RATE_PITCH_D);
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pid_acro_rate_pitch.imax(ACRO_RATE_PITCH_IMAX * 100);
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pid_acro_rate_yaw.kP(ACRO_RATE_YAW_P);
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pid_acro_rate_yaw.kI(ACRO_RATE_YAW_I);
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pid_acro_rate_yaw.kD(ACRO_RATE_YAW_D);
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pid_acro_rate_yaw.imax(ACRO_RATE_YAW_IMAX * 100);
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acro_rate_roll_pitch = ACRO_RATE_RP;
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acro_rate_yaw = ACRO_RATE_YAW;
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// stabilize, angle error
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pid_stabilize_roll.kP(STABILIZE_ROLL_P);
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pid_stabilize_roll.kI(STABILIZE_ROLL_I);
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pid_stabilize_roll.kD(STABILIZE_ROLL_D);
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pid_stabilize_roll.imax(STABILIZE_ROLL_IMAX * 100);
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pid_stabilize_pitch.kP(STABILIZE_PITCH_P);
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pid_stabilize_pitch.kI(STABILIZE_PITCH_I);
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pid_stabilize_pitch.kD(STABILIZE_PITCH_D);
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pid_stabilize_pitch.imax(STABILIZE_PITCH_IMAX * 100);
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// rate control for angle error
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stabilize_rate_roll_pitch = STABILIZE_RATE_RP;
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stabilize_rate_yaw = STABILIZE_RATE_YAW;
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pid_yaw.kP(YAW_P);
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pid_yaw.kI(YAW_I);
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pid_yaw.kD(YAW_D);
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pid_yaw.imax(YAW_IMAX * 100);
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// navigation
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pid_nav.kP(NAV_P);
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pid_nav.kI(NAV_I);
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pid_nav.kD(NAV_D);
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pid_nav.imax(NAV_IMAX * 100);
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pid_throttle.kP(THROTTLE_P);
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pid_throttle.kI(THROTTLE_I);
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pid_throttle.kD(THROTTLE_D);
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pid_throttle.imax(THROTTLE_IMAX * 100);
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save_EEPROM_PID();
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print_done();
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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 = 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
|
|
flight_modes[switchPosition] = mode;
|
|
|
|
// print new mode
|
|
print_switch(switchPosition, mode);
|
|
}
|
|
|
|
// escape hatch
|
|
if(Serial.available() > 0){
|
|
save_EEPROM_flight_modes();
|
|
print_done();
|
|
return (0);
|
|
}
|
|
}
|
|
}
|
|
|
|
|
|
static int8_t
|
|
setup_declination(uint8_t argc, const Menu::arg *argv)
|
|
{
|
|
mag_declination = argv[1].f;
|
|
save_EEPROM_mag_declination();
|
|
read_EEPROM_mag_declination();
|
|
|
|
Serial.printf_P(PSTR("\nsaved: "));
|
|
Serial.println(argv[1].f, 2);
|
|
}
|
|
|
|
static int8_t
|
|
setup_erase(uint8_t argc, const Menu::arg *argv)
|
|
{
|
|
zero_eeprom();
|
|
return 0;
|
|
}
|
|
|
|
|
|
static int8_t
|
|
setup_compass_enable(uint8_t argc, const Menu::arg *argv)
|
|
{
|
|
Serial.printf_P(PSTR("\nCompass enabled:\n"));
|
|
compass_enabled = true;
|
|
save_EEPROM_mag();
|
|
init_compass();
|
|
return 0;
|
|
}
|
|
|
|
static int8_t
|
|
setup_compass_disable(uint8_t argc, const Menu::arg *argv)
|
|
{
|
|
Serial.printf_P(PSTR("\nCompass disabled:\n"));
|
|
compass_enabled = false;
|
|
save_EEPROM_mag();
|
|
return 0;
|
|
}
|
|
|
|
static int8_t
|
|
setup_frame(uint8_t argc, const Menu::arg *argv)
|
|
{
|
|
if(argv[1].i < 1){
|
|
Serial.printf_P(PSTR("\nUsage:\nPlus frame =>frame 1\nX frame =>frame 2\n\n"));
|
|
return 0;
|
|
}
|
|
|
|
if(argv[1].i == 1){
|
|
Serial.printf_P(PSTR("\nSaving Plus frame\n\n"));
|
|
frame_type = PLUS_FRAME;
|
|
|
|
}else if(argv[1].i == 2){
|
|
|
|
Serial.printf_P(PSTR("\nSaving X frame\n\n"));
|
|
frame_type = X_FRAME;
|
|
}
|
|
save_EEPROM_frame();
|
|
return 0;
|
|
}
|
|
|
|
|
|
static int8_t
|
|
setup_compass(uint8_t argc, const Menu::arg *argv)
|
|
{
|
|
Serial.printf_P(PSTR("\nRotate/Pitch/Roll your ArduCopter until the offset variables stop changing.\n"));
|
|
print_hit_enter();
|
|
Serial.printf_P(PSTR("Starting in 3 secs.\n"));
|
|
delay(3000);
|
|
|
|
|
|
compass.init(); // Initialization
|
|
compass.set_orientation(MAGORIENTATION); // set compass's orientation on aircraft
|
|
compass.set_offsets(0, 0, 0); // set offsets to account for surrounding interference
|
|
compass.set_declination(ToRad(DECLINATION)); // set local difference between magnetic north and true north
|
|
//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) {
|
|
deltaMiliSeconds = millis() - fast_loopTimer;
|
|
fast_loopTimer = millis();
|
|
G_Dt = (float)deltaMiliSeconds / 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];
|
|
|
|
save_EEPROM_mag_offset();
|
|
|
|
// set offsets to account for surrounding interference
|
|
compass.set_offsets(mag_offset_x, mag_offset_y, mag_offset_z);
|
|
|
|
print_done();
|
|
break;
|
|
}
|
|
}
|
|
}
|
|
}
|
|
|
|
/***************************************************************************/
|
|
// CLI utilities
|
|
/***************************************************************************/
|
|
|
|
void print_PID(PID * pid)
|
|
{
|
|
Serial.printf_P(PSTR("P: "));
|
|
Serial.print((float)pid->kP(),3);
|
|
Serial.printf_P(PSTR(",I: "));
|
|
Serial.print((float)pid->kI(),3);
|
|
Serial.printf_P(PSTR(",D: "));
|
|
Serial.print((float)pid->kD(),3);
|
|
Serial.printf_P(PSTR(",IMAX: "));
|
|
Serial.println(pid->imax()/100,DEC); // imax is stored as *100 degrees internally
|
|
}
|
|
|
|
void
|
|
print_radio_values()
|
|
{
|
|
Serial.printf_P(PSTR("CH1: %d | %d\n"), rc_1.radio_min, rc_1.radio_max);
|
|
Serial.printf_P(PSTR("CH2: %d | %d\n"), rc_2.radio_min, rc_2.radio_max);
|
|
Serial.printf_P(PSTR("CH3: %d | %d\n"), rc_3.radio_min, rc_3.radio_max);
|
|
Serial.printf_P(PSTR("CH4: %d | %d\n"), rc_4.radio_min, rc_4.radio_max);
|
|
Serial.printf_P(PSTR("CH5: %d | %d\n"), rc_5.radio_min, rc_5.radio_max);
|
|
Serial.printf_P(PSTR("CH6: %d | %d\n"), rc_6.radio_min, rc_6.radio_max);
|
|
Serial.printf_P(PSTR("CH7: %d | %d\n"), rc_7.radio_min, rc_7.radio_max);
|
|
Serial.printf_P(PSTR("CH8: %d | %d\n"), rc_8.radio_min, 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("");
|
|
}
|
|
}
|
|
|
|
|
|
// for reading in vales for mode switch
|
|
boolean
|
|
radio_input_switch(void)
|
|
{
|
|
static byte bouncer;
|
|
|
|
if (abs(rc_1.radio_in - rc_1.radio_trim) > 200)
|
|
bouncer = 10;
|
|
|
|
if (bouncer > 0)
|
|
bouncer--;
|
|
|
|
if (bouncer == 1){
|
|
return true;
|
|
}else{
|
|
return false;
|
|
}
|
|
}
|
|
|
|
|
|
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"));
|
|
}
|