mirror of https://github.com/ArduPilot/ardupilot
Copter: Add support for terrain altitude time constant
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6344faeb29
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7978347044
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@ -137,6 +137,8 @@ const AP_Scheduler::Task Copter::scheduler_tasks[] = {
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FAST_TASK(update_home_from_EKF),
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// check if we've landed or crashed
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FAST_TASK(update_land_and_crash_detectors),
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// surface tracking update
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FAST_TASK(update_rangefinder_terrain_offset),
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#if HAL_MOUNT_ENABLED
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// camera mount's fast update
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FAST_TASK_CLASS(AP_Mount, &copter.camera_mount, update_fast),
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@ -262,6 +262,7 @@ private:
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int16_t alt_cm_glitch_protected; // last glitch protected altitude
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int8_t glitch_count; // non-zero number indicates rangefinder is glitching
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uint32_t glitch_cleared_ms; // system time glitch cleared
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float terrain_offset_cm; // filtered terrain offset (e.g. terrain's height above EKF origin)
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} rangefinder_state, rangefinder_up_state;
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// return rangefinder height interpolated using inertial altitude
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@ -269,6 +270,7 @@ private:
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class SurfaceTracking {
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public:
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// update_surface_offset - manages the vertical offset of the position controller to follow the
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// measured ground or ceiling level measured using the range finder.
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void update_surface_offset();
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@ -900,6 +902,7 @@ private:
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void read_rangefinder(void);
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bool rangefinder_alt_ok() const;
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bool rangefinder_up_ok() const;
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void update_rangefinder_terrain_offset();
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void update_optical_flow(void);
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// takeoff_check.cpp
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@ -1200,6 +1200,14 @@ const AP_Param::GroupInfo ParametersG2::var_info2[] = {
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// @User: Standard
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AP_GROUPINFO("PLDP_SPEED_DN", 4, ParametersG2, pldp_descent_speed_ms, 0.0),
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// @Param: SURFTRAK_TC
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// @DisplayName: Surface Tracking Filter Time Constant
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// @Description: Time to achieve 63.2% of the surface altitude measurement change. If 0 filtering is disabled
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// @Units: s
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// @Range: 0 5
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// @User: Advanced
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AP_GROUPINFO("SURFTRAK_TC", 5, ParametersG2, surftrak_tc, 1.0),
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// ID 62 is reserved for the AP_SUBGROUPEXTENSION
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AP_GROUPEND
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@ -674,6 +674,7 @@ public:
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AP_Int8 surftrak_mode;
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AP_Int8 failsafe_dr_enable;
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AP_Int16 failsafe_dr_timeout;
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AP_Float surftrak_tc;
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// ramp time of throttle during take-off
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AP_Float takeoff_throttle_slew_time;
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@ -74,6 +74,7 @@ void Copter::read_rangefinder(void)
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// clear glitch and record time so consumers (i.e. surface tracking) can reset their target altitudes
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rf_state.glitch_count = 0;
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rf_state.alt_cm_glitch_protected = rf_state.alt_cm;
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rf_state.terrain_offset_cm = rf_state.inertial_alt_cm - rf_state.alt_cm;
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rf_state.glitch_cleared_ms = AP_HAL::millis();
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}
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@ -84,6 +85,7 @@ void Copter::read_rangefinder(void)
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if (timed_out) {
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// reset filter if we haven't used it within the last second
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rf_state.alt_cm_filt.reset(rf_state.alt_cm);
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rf_state.terrain_offset_cm = rf_state.inertial_alt_cm - rf_state.alt_cm;
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} else {
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rf_state.alt_cm_filt.apply(rf_state.alt_cm, 0.05f);
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}
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@ -91,17 +93,13 @@ void Copter::read_rangefinder(void)
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}
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// send downward facing lidar altitude and health to the libraries that require it
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#if HAL_PROXIMITY_ENABLED
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if (rf_orient == ROTATION_PITCH_270) {
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if (rangefinder_state.alt_healthy || timed_out) {
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wp_nav->set_rangefinder_alt(rangefinder_state.enabled, rangefinder_state.alt_healthy, rangefinder_state.alt_cm_filt.get());
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#if MODE_CIRCLE_ENABLED
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circle_nav->set_rangefinder_alt(rangefinder_state.enabled && wp_nav->rangefinder_used(), rangefinder_state.alt_healthy, rangefinder_state.alt_cm_filt.get());
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#endif
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#if HAL_PROXIMITY_ENABLED
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g2.proximity.set_rangefinder_alt(rangefinder_state.enabled, rangefinder_state.alt_healthy, rangefinder_state.alt_cm_filt.get());
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#endif
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}
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}
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#endif
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}
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#else
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@ -129,6 +127,24 @@ bool Copter::rangefinder_up_ok() const
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return (rangefinder_up_state.enabled && rangefinder_up_state.alt_healthy);
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}
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// update rangefinder based terrain offset
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// terrain offset is the terrain's height above the EKF origin
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void Copter::update_rangefinder_terrain_offset()
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{
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float terrain_offset_cm = rangefinder_state.inertial_alt_cm - rangefinder_state.alt_cm_glitch_protected;
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rangefinder_state.terrain_offset_cm += (terrain_offset_cm - rangefinder_state.terrain_offset_cm) * (copter.G_Dt / MAX(copter.g2.surftrak_tc, copter.G_Dt));
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terrain_offset_cm = rangefinder_up_state.inertial_alt_cm + rangefinder_up_state.alt_cm_glitch_protected;
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rangefinder_up_state.terrain_offset_cm += (terrain_offset_cm - rangefinder_up_state.terrain_offset_cm) * (copter.G_Dt / MAX(copter.g2.surftrak_tc, copter.G_Dt));
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if (rangefinder_state.alt_healthy || (AP_HAL::millis() - rangefinder_state.last_healthy_ms > RANGEFINDER_TIMEOUT_MS)) {
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wp_nav->set_rangefinder_terrain_offset(rangefinder_state.enabled, rangefinder_state.alt_healthy, rangefinder_state.terrain_offset_cm);
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#if MODE_CIRCLE_ENABLED
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circle_nav->set_rangefinder_terrain_offset(rangefinder_state.enabled && wp_nav->rangefinder_used(), rangefinder_state.alt_healthy, rangefinder_state.terrain_offset_cm);
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#endif
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}
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}
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/*
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get inertially interpolated rangefinder height. Inertial height is
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recorded whenever we update the rangefinder height, then we use the
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@ -16,11 +16,9 @@ void Copter::SurfaceTracking::update_surface_offset()
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// calculate surfaces height above the EKF origin
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// e.g. if vehicle is 10m above the EKF origin and rangefinder reports alt of 3m. curr_surface_alt_above_origin_cm is 7m (or 700cm)
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RangeFinderState &rf_state = (surface == Surface::GROUND) ? copter.rangefinder_state : copter.rangefinder_up_state;
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const float dir = (surface == Surface::GROUND) ? 1.0f : -1.0f;
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const float curr_surface_alt_above_origin_cm = rf_state.inertial_alt_cm - dir * rf_state.alt_cm_filt.get();
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// update position controller target offset to the surface's alt above the EKF origin
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copter.pos_control->set_pos_offset_target_z_cm(curr_surface_alt_above_origin_cm);
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copter.pos_control->set_pos_offset_target_z_cm(rf_state.terrain_offset_cm);
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last_update_ms = now_ms;
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valid_for_logging = true;
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@ -30,7 +28,7 @@ void Copter::SurfaceTracking::update_surface_offset()
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if (timeout ||
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reset_target ||
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(last_glitch_cleared_ms != rf_state.glitch_cleared_ms)) {
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copter.pos_control->set_pos_offset_z_cm(curr_surface_alt_above_origin_cm);
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copter.pos_control->set_pos_offset_z_cm(rf_state.terrain_offset_cm);
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reset_target = false;
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last_glitch_cleared_ms = rf_state.glitch_cleared_ms;
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}
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