2012-04-30 04:17:14 -03:00
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// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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#ifndef PARAMETERS_H
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#define PARAMETERS_H
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#include <AP_Common.h>
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// Global parameter class.
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//
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class Parameters {
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public:
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// The version of the layout as described by the parameter enum.
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//
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// When changing the parameter enum in an incompatible fashion, this
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// value should be incremented by one.
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//
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// The increment will prevent old parameters from being used incorrectly
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// by newer code.
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//
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2012-11-17 02:45:20 -04:00
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static const uint16_t k_format_version = 14;
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2012-04-30 04:17:14 -03:00
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// The parameter software_type is set up solely for ground station use
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// and identifies the software type (eg ArduPilotMega versus ArduCopterMega)
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// GCS will interpret values 0-9 as ArduPilotMega. Developers may use
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// values within that range to identify different branches.
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//
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2012-05-14 16:21:29 -03:00
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static const uint16_t k_software_type = 20; // 0 for APM trunk
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2012-04-30 04:17:14 -03:00
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enum {
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// Layout version number, always key zero.
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//
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k_param_format_version = 0,
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k_param_software_type,
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// Misc
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//
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k_param_auto_trim,
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k_param_switch_enable,
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k_param_log_bitmask,
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2012-11-27 17:58:11 -04:00
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k_param_mix_mode, // unused
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k_param_reverse_elevons, // unused
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k_param_reverse_ch1_elevon, // unused
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k_param_reverse_ch2_elevon, // unused
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k_param_flap_1_percent, // unused
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k_param_flap_1_speed, // unused
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k_param_flap_2_percent, // unused
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k_param_flap_2_speed, // unused
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2012-04-30 04:17:14 -03:00
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k_param_num_resets,
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k_param_log_last_filenumber, // *** Deprecated - remove with next eeprom number change
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k_param_reset_switch_chan,
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2012-11-07 03:28:20 -04:00
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k_param_manual_level,
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k_param_ins, // libraries/AP_InertialSensor variables
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2012-12-18 07:44:12 -04:00
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k_param_rssi_pin,
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k_param_battery_volt_pin,
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k_param_battery_curr_pin,
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2012-04-30 04:17:14 -03:00
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// 110: Telemetry control
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//
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k_param_gcs0 = 110, // stream rates for port0
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k_param_gcs3, // stream rates for port3
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k_param_sysid_this_mav,
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k_param_sysid_my_gcs,
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k_param_serial3_baud,
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2012-08-29 20:36:18 -03:00
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k_param_telem_delay,
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2012-04-30 04:17:14 -03:00
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// 120: Fly-by-wire control
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//
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k_param_flybywire_airspeed_min = 120,
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k_param_flybywire_airspeed_max,
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k_param_FBWB_min_altitude, // 0=disabled, minimum value for altitude in cm (for first time try 30 meters = 3000 cm)
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//
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// 130: Sensor parameters
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//
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2012-11-07 03:28:20 -04:00
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k_param_imu = 130,
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k_param_altitude_mix, // sensor calibration
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2012-04-30 04:17:14 -03:00
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k_param_airspeed_ratio,
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k_param_ground_temperature,
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k_param_ground_pressure,
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k_param_compass_enabled,
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k_param_compass,
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k_param_battery_monitoring,
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k_param_volt_div_ratio,
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k_param_curr_amp_per_volt,
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k_param_input_voltage,
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k_param_pack_capacity,
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k_param_airspeed_offset,
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2012-05-14 12:47:08 -03:00
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#if HIL_MODE != HIL_MODE_ATTITUDE
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2012-06-13 03:29:32 -03:00
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#if CONFIG_SONAR == ENABLED
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2012-05-14 12:47:08 -03:00
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k_param_sonar_enabled,
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k_param_sonar_type,
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#endif
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#endif
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2012-11-17 02:45:20 -04:00
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k_param_ahrs, // AHRS group
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2012-04-30 04:17:14 -03:00
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//
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// 150: Navigation parameters
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//
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k_param_crosstrack_gain = 150,
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k_param_crosstrack_entry_angle,
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k_param_roll_limit,
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k_param_pitch_limit_max,
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k_param_pitch_limit_min,
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k_param_airspeed_cruise,
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k_param_min_gndspeed,
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k_param_ch7_option,
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//
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// 160: Radio settings
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//
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k_param_channel_roll = 160,
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k_param_channel_pitch,
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k_param_channel_throttle,
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k_param_channel_rudder,
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k_param_rc_5,
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k_param_rc_6,
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k_param_rc_7,
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k_param_rc_8,
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k_param_throttle_min,
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k_param_throttle_max,
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k_param_throttle_fs_enabled, // 170
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k_param_throttle_fs_value,
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k_param_throttle_cruise,
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k_param_short_fs_action,
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k_param_long_fs_action,
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2012-11-27 19:42:10 -04:00
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k_param_gcs_heartbeat_fs_enabled,
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2012-04-30 04:17:14 -03:00
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k_param_throttle_slewrate,
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// ************************************************************
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// 180: APMrover parameters - JLN update
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2012-11-27 19:42:10 -04:00
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k_param_closed_loop_nav, // unused
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2012-04-30 04:17:14 -03:00
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k_param_auto_wp_radius,
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k_param_sonar_trigger,
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2012-04-30 04:17:14 -03:00
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k_param_turn_gain,
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k_param_booster,
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// ************************************************************
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//
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// 200: Feed-forward gains
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//
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2012-11-27 20:42:51 -04:00
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k_param_kff_pitch_compensation = 200, // unused
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k_param_kff_rudder_mix, // unused
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k_param_kff_pitch_to_throttle, // unused
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k_param_kff_throttle_to_pitch, // unused
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2012-04-30 04:17:14 -03:00
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//
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// 210: flight modes
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//
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k_param_flight_mode_channel = 210,
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k_param_flight_mode1,
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k_param_flight_mode2,
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k_param_flight_mode3,
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k_param_flight_mode4,
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k_param_flight_mode5,
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k_param_flight_mode6,
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//
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// 220: Waypoint data
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//
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k_param_waypoint_mode = 220,
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k_param_command_total,
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k_param_command_index,
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k_param_waypoint_radius,
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k_param_loiter_radius, // unused
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k_param_fence_action,
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k_param_fence_total,
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k_param_fence_channel,
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k_param_fence_minalt,
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k_param_fence_maxalt,
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2012-11-27 08:20:25 -04:00
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// other objects
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k_param_sitl = 230,
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2012-04-30 04:17:14 -03:00
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//
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// 240: PID Controllers
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//
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// Heading-to-roll PID:
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// heading error from command to roll command deviation from trim
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// (bank to turn strategy)
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//
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k_param_pidNavRoll = 240,
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// Roll-to-servo PID:
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// roll error from command to roll servo deviation from trim
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// (tracks commanded bank angle)
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//
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k_param_pidServoRoll,
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//
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// Pitch control
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//
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// Pitch-to-servo PID:
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// pitch error from command to pitch servo deviation from trim
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// (front-side strategy)
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//
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k_param_pidServoPitch,
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// Airspeed-to-pitch PID:
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// airspeed error from command to pitch servo deviation from trim
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// (back-side strategy)
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//
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k_param_pidNavPitchAirspeed,
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//
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// Yaw control
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//
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// Yaw-to-servo PID:
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// yaw rate error from command to yaw servo deviation from trim
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// (stabilizes dutch roll)
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//
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k_param_pidServoRudder,
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//
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// Throttle control
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//
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// Energy-to-throttle PID:
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// total energy error from command to throttle servo deviation from trim
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// (throttle back-side strategy alternative)
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//
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k_param_pidTeThrottle,
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// Altitude-to-pitch PID:
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// altitude error from command to pitch servo deviation from trim
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// (throttle front-side strategy alternative)
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//
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k_param_pidNavPitchAltitude,
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// 254,255: reserved
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};
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AP_Int16 format_version;
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AP_Int8 software_type;
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// Telemetry control
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//
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AP_Int16 sysid_this_mav;
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AP_Int16 sysid_my_gcs;
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AP_Int8 serial3_baud;
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2012-08-29 20:36:18 -03:00
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AP_Int8 telem_delay;
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2012-04-30 04:17:14 -03:00
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// Crosstrack navigation
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//
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AP_Float crosstrack_gain;
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AP_Int16 crosstrack_entry_angle;
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// Estimation
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//
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AP_Float altitude_mix;
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AP_Float airspeed_ratio;
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AP_Int16 airspeed_offset;
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// Waypoints
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//
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AP_Int8 waypoint_mode;
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AP_Int8 command_total;
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AP_Int8 command_index;
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AP_Int8 waypoint_radius;
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// Fly-by-wire
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//
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AP_Int8 flybywire_airspeed_min;
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AP_Int8 flybywire_airspeed_max;
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AP_Int16 FBWB_min_altitude;
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// Throttle
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//
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AP_Int8 throttle_min;
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AP_Int8 throttle_max;
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AP_Int8 throttle_slewrate;
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AP_Int8 throttle_fs_enabled;
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AP_Int16 throttle_fs_value;
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AP_Int8 throttle_cruise;
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// Failsafe
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AP_Int8 short_fs_action;
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AP_Int8 long_fs_action;
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AP_Int8 gcs_heartbeat_fs_enabled;
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// Flight modes
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//
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AP_Int8 flight_mode_channel;
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AP_Int8 flight_mode1;
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AP_Int8 flight_mode2;
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AP_Int8 flight_mode3;
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AP_Int8 flight_mode4;
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AP_Int8 flight_mode5;
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AP_Int8 flight_mode6;
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// Navigational maneuvering limits
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//
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AP_Int16 roll_limit;
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AP_Int16 pitch_limit_max;
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AP_Int16 pitch_limit_min;
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// Misc
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//
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AP_Int8 auto_trim;
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AP_Int16 num_resets;
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AP_Int16 log_bitmask;
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AP_Int16 log_last_filenumber; // *** Deprecated - remove with next eeprom number change
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AP_Int8 reset_switch_chan;
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AP_Int8 manual_level;
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AP_Int16 airspeed_cruise;
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AP_Int16 min_gndspeed;
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AP_Int8 ch7_option;
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AP_Int16 ground_temperature;
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AP_Int32 ground_pressure;
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AP_Int8 compass_enabled;
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AP_Int16 angle_of_attack;
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AP_Int8 battery_monitoring; // 0=disabled, 3=voltage only, 4=voltage and current
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AP_Float volt_div_ratio;
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AP_Float curr_amp_per_volt;
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AP_Float input_voltage;
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2012-12-18 07:44:12 -04:00
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AP_Int16 pack_capacity; // Battery pack capacity less reserve
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AP_Int8 rssi_pin;
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AP_Int8 battery_volt_pin;
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AP_Int8 battery_curr_pin;
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2012-05-14 12:47:08 -03:00
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#if HIL_MODE != HIL_MODE_ATTITUDE
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2012-06-13 03:29:32 -03:00
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#if CONFIG_SONAR == ENABLED
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2012-05-14 12:47:08 -03:00
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AP_Int8 sonar_enabled;
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2012-07-11 22:46:47 -03:00
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AP_Int8 sonar_type; // 0 = XL, 1 = LV,
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// 2 = XLL (XL with 10m range)
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// 3 = HRLV
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2012-05-14 12:47:08 -03:00
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#endif
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#endif
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2012-04-30 04:17:14 -03:00
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// ************ ThermoPilot parameters ************************
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// - JLN update
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AP_Int8 auto_wp_radius;
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2012-05-14 12:47:08 -03:00
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AP_Int16 sonar_trigger;
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2012-04-30 04:17:14 -03:00
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AP_Int16 turn_gain;
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2012-05-17 13:42:16 -03:00
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AP_Int8 booster;
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2012-04-30 04:17:14 -03:00
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// ************************************************************
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// RC channels
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2012-08-06 22:24:20 -03:00
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RC_Channel channel_roll;
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RC_Channel channel_pitch;
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RC_Channel channel_throttle;
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RC_Channel channel_rudder;
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RC_Channel_aux rc_5;
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RC_Channel_aux rc_6;
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RC_Channel_aux rc_7;
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RC_Channel_aux rc_8;
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2012-04-30 04:17:14 -03:00
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// PID controllers
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//
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PID pidNavRoll;
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PID pidServoRoll;
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PID pidServoPitch;
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PID pidNavPitchAirspeed;
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PID pidServoRudder;
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PID pidTeThrottle;
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PID pidNavPitchAltitude;
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Parameters() :
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2012-08-06 22:24:20 -03:00
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// RC channels
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channel_roll(CH_1),
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channel_pitch(CH_2),
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channel_throttle(CH_3),
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channel_rudder(CH_4),
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rc_5(CH_5),
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rc_6(CH_6),
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rc_7(CH_7),
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rc_8(CH_8),
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2012-04-30 04:17:14 -03:00
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// PID controller initial P initial I initial D initial imax
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//-----------------------------------------------------------------------------------
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pidNavRoll (NAV_ROLL_P, NAV_ROLL_I, NAV_ROLL_D, NAV_ROLL_INT_MAX_CENTIDEGREE),
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pidServoRoll (SERVO_ROLL_P, SERVO_ROLL_I, SERVO_ROLL_D, SERVO_ROLL_INT_MAX_CENTIDEGREE),
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pidServoPitch (SERVO_PITCH_P, SERVO_PITCH_I, SERVO_PITCH_D, SERVO_PITCH_INT_MAX_CENTIDEGREE),
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pidNavPitchAirspeed (NAV_PITCH_ASP_P, NAV_PITCH_ASP_I, NAV_PITCH_ASP_D, NAV_PITCH_ASP_INT_MAX_CMSEC),
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pidServoRudder (SERVO_YAW_P, SERVO_YAW_I, SERVO_YAW_D, SERVO_YAW_INT_MAX),
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pidTeThrottle (THROTTLE_TE_P, THROTTLE_TE_I, THROTTLE_TE_D, THROTTLE_TE_INT_MAX),
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pidNavPitchAltitude (NAV_PITCH_ALT_P, NAV_PITCH_ALT_I, NAV_PITCH_ALT_D, NAV_PITCH_ALT_INT_MAX_CM)
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{}
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};
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2012-08-06 22:24:20 -03:00
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extern const AP_Param::Info var_info[];
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2012-04-30 04:17:14 -03:00
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#endif // PARAMETERS_H
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