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228 lines
8.5 KiB
228 lines
8.5 KiB
#include "Copter.h" |
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// Traditional helicopter variables and functions |
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#if FRAME_CONFIG == HELI_FRAME |
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#ifndef HELI_DYNAMIC_FLIGHT_SPEED_MIN |
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#define HELI_DYNAMIC_FLIGHT_SPEED_MIN 500 // we are in "dynamic flight" when the speed is over 5m/s for 2 seconds |
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#endif |
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// counter to control dynamic flight profile |
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static int8_t heli_dynamic_flight_counter; |
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// heli_init - perform any special initialisation required for the tradheli |
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void Copter::heli_init() |
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{ |
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// pre-load stab col values as mode is initialized as Stabilize, but stabilize_init() function is not run on start-up. |
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input_manager.set_use_stab_col(true); |
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input_manager.set_stab_col_ramp(1.0); |
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} |
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// heli_check_dynamic_flight - updates the dynamic_flight flag based on our horizontal velocity |
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// should be called at 50hz |
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void Copter::check_dynamic_flight(void) |
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{ |
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if (motors->get_spool_state() != AP_Motors::SpoolState::THROTTLE_UNLIMITED || |
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flightmode->is_landing()) { |
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heli_dynamic_flight_counter = 0; |
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heli_flags.dynamic_flight = false; |
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return; |
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} |
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bool moving = false; |
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// with GPS lock use inertial nav to determine if we are moving |
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if (position_ok()) { |
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// get horizontal speed |
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const float speed = inertial_nav.get_speed_xy(); |
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moving = (speed >= HELI_DYNAMIC_FLIGHT_SPEED_MIN); |
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}else{ |
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// with no GPS lock base it on throttle and forward lean angle |
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moving = (motors->get_throttle() > 0.8f || ahrs.pitch_sensor < -1500); |
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} |
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if (!moving && rangefinder_state.enabled && rangefinder.status_orient(ROTATION_PITCH_270) == RangeFinder::Status::Good) { |
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// when we are more than 2m from the ground with good |
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// rangefinder lock consider it to be dynamic flight |
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moving = (rangefinder.distance_cm_orient(ROTATION_PITCH_270) > 200); |
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} |
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if (moving) { |
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// if moving for 2 seconds, set the dynamic flight flag |
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if (!heli_flags.dynamic_flight) { |
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heli_dynamic_flight_counter++; |
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if (heli_dynamic_flight_counter >= 100) { |
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heli_flags.dynamic_flight = true; |
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heli_dynamic_flight_counter = 100; |
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} |
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} |
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}else{ |
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// if not moving for 2 seconds, clear the dynamic flight flag |
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if (heli_flags.dynamic_flight) { |
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if (heli_dynamic_flight_counter > 0) { |
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heli_dynamic_flight_counter--; |
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}else{ |
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heli_flags.dynamic_flight = false; |
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} |
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} |
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} |
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} |
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// update_heli_control_dynamics - pushes several important factors up into AP_MotorsHeli. |
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// should be run between the rate controller and the servo updates. |
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void Copter::update_heli_control_dynamics(void) |
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{ |
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// Use Leaky_I if we are not moving fast |
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attitude_control->use_leaky_i(!heli_flags.dynamic_flight); |
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if (ap.land_complete || (is_zero(motors->get_desired_rotor_speed()))){ |
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// if we are landed or there is no rotor power demanded, decrement slew scalar |
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hover_roll_trim_scalar_slew--; |
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} else { |
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// if we are not landed and motor power is demanded, increment slew scalar |
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hover_roll_trim_scalar_slew++; |
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} |
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hover_roll_trim_scalar_slew = constrain_int16(hover_roll_trim_scalar_slew, 0, scheduler.get_loop_rate_hz()); |
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// set hover roll trim scalar, will ramp from 0 to 1 over 1 second after we think helicopter has taken off |
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attitude_control->set_hover_roll_trim_scalar((float) hover_roll_trim_scalar_slew/(float) scheduler.get_loop_rate_hz()); |
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} |
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bool Copter::should_use_landing_swash() const |
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{ |
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if (flightmode->has_manual_throttle() || |
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control_mode == Mode::Number::DRIFT) { |
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// manual modes always uses full swash range |
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return false; |
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} |
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if (flightmode->is_landing()) { |
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// landing with non-manual throttle mode always uses limit swash range |
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return true; |
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} |
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if (ap.land_complete) { |
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// when landed in non-manual throttle mode limit swash range |
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return true; |
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} |
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if (!ap.auto_armed) { |
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// when waiting to takeoff in non-manual throttle mode limit swash range |
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return true; |
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} |
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if (!heli_flags.dynamic_flight) { |
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// Just in case we are unsure of being in non-manual throttle |
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// mode, limit swash range in low speed and hovering flight. |
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// This will catch any non-manual throttle mode attempting a |
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// landing and driving the collective too low before the land |
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// complete flag is set. |
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return true; |
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} |
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return false; |
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} |
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// heli_update_landing_swash - sets swash plate flag so higher minimum is used when landed or landing |
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// should be called soon after update_land_detector in main code |
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void Copter::heli_update_landing_swash() |
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{ |
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motors->set_collective_for_landing(should_use_landing_swash()); |
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} |
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// convert motor interlock switch's position to desired rotor speed expressed as a value from 0 to 1 |
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// returns zero if motor interlock auxiliary switch hasn't been defined |
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float Copter::get_pilot_desired_rotor_speed() const |
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{ |
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RC_Channel *rc_ptr = rc().find_channel_for_option(RC_Channel::AUX_FUNC::MOTOR_INTERLOCK); |
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if (rc_ptr != nullptr) { |
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rc_ptr->set_range(1000); |
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return (float)rc_ptr->get_control_in() * 0.001f; |
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} |
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return 0.0f; |
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} |
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// heli_update_rotor_speed_targets - reads pilot input and passes new rotor speed targets to heli motors object |
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void Copter::heli_update_rotor_speed_targets() |
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{ |
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static bool rotor_runup_complete_last = false; |
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// get rotor control method |
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uint8_t rsc_control_mode = motors->get_rsc_mode(); |
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switch (rsc_control_mode) { |
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case ROTOR_CONTROL_MODE_SPEED_PASSTHROUGH: |
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// pass through pilot desired rotor speed from the RC |
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if (get_pilot_desired_rotor_speed() > 0.01) { |
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ap.motor_interlock_switch = true; |
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motors->set_desired_rotor_speed(get_pilot_desired_rotor_speed()); |
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} else { |
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ap.motor_interlock_switch = false; |
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motors->set_desired_rotor_speed(0.0f); |
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} |
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break; |
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case ROTOR_CONTROL_MODE_SPEED_SETPOINT: |
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case ROTOR_CONTROL_MODE_OPEN_LOOP_POWER_OUTPUT: |
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case ROTOR_CONTROL_MODE_CLOSED_LOOP_POWER_OUTPUT: |
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// pass setpoint through as desired rotor speed. Needs work, this is pointless as it is |
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// not used by closed loop control. Being used as a catch-all for other modes regardless |
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// of whether or not they actually use it |
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// set rpm from rotor speed sensor |
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if (motors->get_interlock()) { |
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#if RPM_ENABLED == ENABLED |
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float rpm = -1; |
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rpm_sensor.get_rpm(0, rpm); |
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motors->set_rpm(rpm); |
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#endif |
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motors->set_desired_rotor_speed(motors->get_rsc_setpoint()); |
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}else{ |
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motors->set_desired_rotor_speed(0.0f); |
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} |
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break; |
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} |
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// when rotor_runup_complete changes to true, log event |
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if (!rotor_runup_complete_last && motors->rotor_runup_complete()){ |
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AP::logger().Write_Event(LogEvent::ROTOR_RUNUP_COMPLETE); |
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} else if (rotor_runup_complete_last && !motors->rotor_runup_complete()){ |
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AP::logger().Write_Event(LogEvent::ROTOR_SPEED_BELOW_CRITICAL); |
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} |
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rotor_runup_complete_last = motors->rotor_runup_complete(); |
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} |
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// heli_update_autorotation - determines if aircraft is in autorotation and sets motors flag and switches |
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// to autorotation flight mode if manual collective is not being used. |
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void Copter::heli_update_autorotation() |
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{ |
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#if MODE_AUTOROTATE_ENABLED == ENABLED |
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// check if flying and interlock disengaged |
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if (!ap.land_complete && !motors->get_interlock()) { |
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if (!flightmode->has_manual_throttle() && g2.arot.is_enable()) { |
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// set autonomous autorotation flight mode |
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set_mode(Mode::Number::AUTOROTATE, ModeReason::AUTOROTATION_START); |
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} |
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// set flag to facilitate both auto and manual autorotations |
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heli_flags.in_autorotation = true; |
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} else { |
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heli_flags.in_autorotation = false; |
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} |
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// sets autorotation flags through out libraries |
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heli_set_autorotation(heli_flags.in_autorotation); |
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if (!ap.land_complete) { |
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motors->set_enable_bailout(true); |
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} else { |
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motors->set_enable_bailout(false); |
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} |
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#else |
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heli_flags.in_autorotation = false; |
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motors->set_enable_bailout(false); |
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#endif |
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} |
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#if MODE_AUTOROTATE_ENABLED == ENABLED |
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// heli_set_autorotation - set the autorotation flag throughout libraries |
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void Copter::heli_set_autorotation(bool autorotation) |
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{ |
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motors->set_in_autorotation(autorotation); |
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} |
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#endif |
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#endif // FRAME_CONFIG == HELI_FRAME
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