9141ad2825
- Fleshed out the original idea to completely remove the long slope at the end of deceleration issue. This third time should absolutely eliminate it. - Changed the acceleration setting to kept as mm/min^2 internally, since this was creating unneccessary additional computation in the planner. Human readable value kept at mm/sec^2. - Updated grbl version 0.7d and settings version to 4. NOTE: Please check settings after update. These may have changed, but shouldn't. - Before updating the new features (pause, e-stop, federate override, etc), the edge branch will soon be merged with the master, barring any immediate issues that people may have, and the edge branch will be the testing ground for the new grbl version 0.8.
207 lines
9.0 KiB
C
207 lines
9.0 KiB
C
/*
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motion_control.c - high level interface for issuing motion commands
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Part of Grbl
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Copyright (c) 2009-2011 Simen Svale Skogsrud
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Copyright (c) 2011 Sungeun K. Jeon
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Grbl is free software: you can redistribute it and/or modify
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it under the terms of the GNU General Public License as published by
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the Free Software Foundation, either version 3 of the License, or
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(at your option) any later version.
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Grbl is distributed in the hope that it will be useful,
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but WITHOUT ANY WARRANTY; without even the implied warranty of
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MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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GNU General Public License for more details.
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You should have received a copy of the GNU General Public License
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along with Grbl. If not, see <http://www.gnu.org/licenses/>.
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*/
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#include <avr/io.h>
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#include "settings.h"
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#include "config.h"
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#include "motion_control.h"
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#include <util/delay.h>
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#include <math.h>
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#include <stdlib.h>
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#include "nuts_bolts.h"
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#include "stepper.h"
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#include "planner.h"
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// Execute dwell in seconds. Maximum time delay is > 18 hours, more than enough for any application.
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void mc_dwell(double seconds)
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{
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uint16_t i = floor(seconds);
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st_synchronize();
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_delay_ms(floor(1000*(seconds-i))); // Delay millisecond remainder
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while (i > 0) {
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_delay_ms(1000); // Delay one second
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i--;
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}
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}
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// void mc_jog_enable()
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// {
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// // Planned sequence of events:
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// // Send X,Y,Z motion, target step rate, direction
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// // Rate_delta, step_xyz, counter_xyz should be all the same.
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// //
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// Change of direction can cause some problems. Need to force a complete stop for any direction change.
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// This likely needs to be done in stepper.c as a jog mode parameter.
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// !!! Need a way to get step locations realtime!!!
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// Jog is a specialized case, where grbl is reset and there is no cycle start.
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// If there is a real-time status elsewhere, this shouldn't be a problem.
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// st.direction_bits = current_block->direction_bits;
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// st.target_rate;
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// st.rate_delta;
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// st.step_event_count;
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// st.steps_x;
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// st.steps_y;
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// st.steps_z;
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// st.counter_x = -(current_block->step_event_count >> 1);
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// st.counter_y = st.counter_x;
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// st.counter_z = st.counter_x;
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// st.step_event_count = current_block->step_event_count;
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// st.step_events_completed = 0;
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// }
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// void mc_jog_disable()
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// {
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// // Calls stepper.c and disables jog mode to start deceleration.
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// // Shouldn't have to anything else. Just initiate the stop, so if re-enabled, it can accelerate.
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// }
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// void mc_feed_hold()
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// {
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// // Planned sequence of events:
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// // Query stepper for interrupting cycle and hold until pause flag is set?
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// // Query stepper intermittenly and check for !st.do_motion to indicate complete stop.
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// // Retreive st.step_events_completed and recompute current location.
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// // Truncate current block start to current location.
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// // Re-plan buffer for start from zero velocity and truncated block length.
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// // All necessary computations for a restart should be done by now.
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// // Reset pause flag.
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// // Only wait for a cycle start command from user interface. (TBD).
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// // !!! Need to check how to circumvent the wait in the main program. May need to be in serial.c
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// // as an interrupt process call. Can two interrupt programs exist at the same time??
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// }
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// Execute an arc in offset mode format. position == current xyz, target == target xyz,
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// offset == offset from current xyz, axis_XXX defines circle plane in tool space, axis_linear is
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// the direction of helical travel, radius == circle radius, isclockwise boolean. Used
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// for vector transformation direction.
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// position, target, and offset are pointers to vectors from gcode.c
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#ifdef __AVR_ATmega328P__
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// The arc is approximated by generating a huge number of tiny, linear segments. The length of each
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// segment is configured in settings.mm_per_arc_segment.
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void mc_arc(double *position, double *target, double *offset, uint8_t axis_0, uint8_t axis_1,
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uint8_t axis_linear, double feed_rate, uint8_t invert_feed_rate, double radius, uint8_t isclockwise)
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{
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// int acceleration_manager_was_enabled = plan_is_acceleration_manager_enabled();
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// plan_set_acceleration_manager_enabled(false); // disable acceleration management for the duration of the arc
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double center_axis0 = position[axis_0] + offset[axis_0];
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double center_axis1 = position[axis_1] + offset[axis_1];
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double linear_travel = target[axis_linear] - position[axis_linear];
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double r_axis0 = -offset[axis_0]; // Radius vector from center to current location
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double r_axis1 = -offset[axis_1];
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double rt_axis0 = target[axis_0] - center_axis0;
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double rt_axis1 = target[axis_1] - center_axis1;
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// CCW angle between position and target from circle center. Only one atan2() trig computation required.
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double angular_travel = atan2(r_axis0*rt_axis1-r_axis1*rt_axis0, r_axis0*rt_axis0+r_axis1*rt_axis1);
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if (angular_travel < 0) { angular_travel += 2*M_PI; }
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if (isclockwise) { angular_travel -= 2*M_PI; }
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double millimeters_of_travel = hypot(angular_travel*radius, fabs(linear_travel));
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if (millimeters_of_travel == 0.0) { return; }
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uint16_t segments = floor(millimeters_of_travel/settings.mm_per_arc_segment);
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// Multiply inverse feed_rate to compensate for the fact that this movement is approximated
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// by a number of discrete segments. The inverse feed_rate should be correct for the sum of
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// all segments.
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if (invert_feed_rate) { feed_rate *= segments; }
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double theta_per_segment = angular_travel/segments;
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double linear_per_segment = linear_travel/segments;
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/* Vector rotation by transformation matrix: r is the original vector, r_T is the rotated vector,
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and phi is the angle of rotation. Based on the solution approach by Jens Geisler.
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r_T = [cos(phi) -sin(phi);
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sin(phi) cos(phi] * r ;
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For arc generation, the center of the circle is the axis of rotation and the radius vector is
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defined from the circle center to the initial position. Each line segment is formed by successive
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vector rotations. This requires only two cos() and sin() computations to form the rotation
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matrix for the duration of the entire arc. Error may accumulate from numerical round-off, since
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all double numbers are single precision on the Arduino. (True double precision will not have
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round off issues for CNC applications.) Single precision error can accumulate to be greater than
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tool precision in some cases. Therefore, arc path correction is implemented.
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Small angle approximation may be used to reduce computation overhead further. This approximation
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holds for everything, but very small circles and large mm_per_arc_segment values. In other words,
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theta_per_segment would need to be greater than 0.1 rad and N_ARC_CORRECTION would need to be large
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to cause an appreciable drift error. N_ARC_CORRECTION~=25 is more than small enough to correct for
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numerical drift error. N_ARC_CORRECTION may be on the order a hundred(s) before error becomes an
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issue for CNC machines with the single precision Arduino calculations.
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This approximation also allows mc_arc to immediately insert a line segment into the planner
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without the initial overhead of computing cos() or sin(). By the time the arc needs to be applied
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a correction, the planner should have caught up to the lag caused by the initial mc_arc overhead.
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This is important when there are successive arc motions.
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*/
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// Vector rotation matrix values
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double cos_T = 1-0.5*theta_per_segment*theta_per_segment; // Small angle approximation
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double sin_T = theta_per_segment;
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double arc_target[3];
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double sin_Ti;
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double cos_Ti;
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double r_axisi;
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uint16_t i;
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int8_t count = 0;
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// Initialize the linear axis
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arc_target[axis_linear] = position[axis_linear];
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for (i = 1; i<segments; i++) { // Increment (segments-1)
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if (count < N_ARC_CORRECTION) {
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// Apply vector rotation matrix
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r_axisi = r_axis0*sin_T + r_axis1*cos_T;
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r_axis0 = r_axis0*cos_T - r_axis1*sin_T;
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r_axis1 = r_axisi;
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count++;
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} else {
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// Arc correction to radius vector. Computed only every N_ARC_CORRECTION increments.
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// Compute exact location by applying transformation matrix from initial radius vector(=-offset).
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cos_Ti = cos(i*theta_per_segment);
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sin_Ti = sin(i*theta_per_segment);
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r_axis0 = -offset[axis_0]*cos_Ti + offset[axis_1]*sin_Ti;
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r_axis1 = -offset[axis_0]*sin_Ti - offset[axis_1]*cos_Ti;
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count = 0;
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}
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// Update arc_target location
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arc_target[axis_0] = center_axis0 + r_axis0;
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arc_target[axis_1] = center_axis1 + r_axis1;
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arc_target[axis_linear] += linear_per_segment;
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plan_buffer_line(arc_target[X_AXIS], arc_target[Y_AXIS], arc_target[Z_AXIS], feed_rate, invert_feed_rate);
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}
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// Ensure last segment arrives at target location.
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plan_buffer_line(target[X_AXIS], target[Y_AXIS], target[Z_AXIS], feed_rate, invert_feed_rate);
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// plan_set_acceleration_manager_enabled(acceleration_manager_was_enabled);
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}
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#endif
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void mc_go_home()
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{
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st_go_home();
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} |