mirror of https://github.com/ArduPilot/ardupilot
204 lines
6.2 KiB
C++
204 lines
6.2 KiB
C++
/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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//
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// Unit tests for the AP_Math rotations code
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//
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#include <AP_HAL.h>
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#include <stdlib.h>
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#include <AP_Common.h>
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#include <AP_Progmem.h>
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#include <AP_Param.h>
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#include <AP_HAL_AVR.h>
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#include <AP_HAL_SITL.h>
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#include <AP_HAL_Empty.h>
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#include <AP_HAL_PX4.h>
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#include <AP_HAL_Linux.h>
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#include <AP_Math.h>
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#include <Filter.h>
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#include <AP_ADC.h>
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#include <SITL.h>
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#include <AP_Compass.h>
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#include <AP_Baro.h>
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#include <AP_Notify.h>
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#include <AP_InertialSensor.h>
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#include <AP_GPS.h>
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#include <DataFlash.h>
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#include <GCS_MAVLink.h>
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#include <AP_Mission.h>
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#include <StorageManager.h>
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#include <AP_Terrain.h>
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#include <AP_Declination.h> // ArduPilot Mega Declination Helper Library
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#include <AP_AHRS.h>
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#include <AP_NavEKF.h>
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#include <AP_Airspeed.h>
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#include <AP_Vehicle.h>
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#include <AP_ADC_AnalogSource.h>
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#include <AP_Rally.h>
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#include <AP_BattMonitor.h>
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#include <AP_RangeFinder.h>
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#include <AP_OpticalFlow.h>
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const AP_HAL::HAL& hal = AP_HAL_BOARD_DRIVER;
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static void print_vector(Vector3f &v)
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{
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hal.console->printf("[%.4f %.4f %.4f]\n",
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v.x, v.y, v.z);
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}
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// test rotation method accuracy
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static void test_rotation_accuracy(void)
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{
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Matrix3f attitude;
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Vector3f small_rotation;
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float roll, pitch, yaw;
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int16_t i;
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float rot_angle;
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hal.console->println_P(PSTR("\nRotation method accuracy:"));
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for( i=0; i<90; i++ ) {
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// reset initial attitude
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attitude.from_euler(0,0,0);
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// calculate small rotation vector
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rot_angle = ToRad(i);
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small_rotation = Vector3f(0,0,rot_angle);
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// apply small rotation
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attitude.rotate(small_rotation);
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// get resulting attitude's euler angles
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attitude.to_euler(&roll, &pitch, &yaw);
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// display results
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hal.console->printf_P(
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PSTR("actual angle: %d\tcalculated angle:%4.2f\n"),
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(int)i,ToDeg(yaw));
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}
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}
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static void test_euler(enum Rotation rotation, float roll, float pitch, float yaw)
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{
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Vector3f v, v1, v2, diff;
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Matrix3f rotmat;
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const float accuracy = 1.0e-6f;
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v.x = 1;
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v.y = 2;
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v.z = 3;
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v1 = v;
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v1.rotate(rotation);
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rotmat.from_euler(radians(roll), radians(pitch), radians(yaw));
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v2 = v;
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v2 = rotmat * v2;
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diff = (v2 - v1);
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if (diff.length() > accuracy) {
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hal.console->printf("euler test %u failed : yaw:%d roll:%d pitch:%d\n",
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(unsigned)rotation,
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(int)yaw,
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(int)roll,
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(int)pitch);
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hal.console->printf("fast rotated: ");
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print_vector(v1);
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hal.console->printf("slow rotated: ");
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print_vector(v2);
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hal.console->printf("\n");
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}
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}
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static void test_eulers(void)
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{
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hal.console->println("euler tests");
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test_euler(ROTATION_NONE, 0, 0, 0);
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test_euler(ROTATION_YAW_45, 0, 0, 45);
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test_euler(ROTATION_YAW_90, 0, 0, 90);
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test_euler(ROTATION_YAW_135, 0, 0, 135);
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test_euler(ROTATION_YAW_180, 0, 0, 180);
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test_euler(ROTATION_YAW_225, 0, 0, 225);
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test_euler(ROTATION_YAW_270, 0, 0, 270);
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test_euler(ROTATION_YAW_315, 0, 0, 315);
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test_euler(ROTATION_ROLL_180, 180, 0, 0);
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test_euler(ROTATION_ROLL_180_YAW_45, 180, 0, 45);
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test_euler(ROTATION_ROLL_180_YAW_90, 180, 0, 90);
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test_euler(ROTATION_ROLL_180_YAW_135, 180, 0, 135);
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test_euler(ROTATION_PITCH_180, 0, 180, 0);
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test_euler(ROTATION_ROLL_180_YAW_225, 180, 0, 225);
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test_euler(ROTATION_ROLL_180_YAW_270, 180, 0, 270);
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test_euler(ROTATION_ROLL_180_YAW_315, 180, 0, 315);
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test_euler(ROTATION_ROLL_90, 90, 0, 0);
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test_euler(ROTATION_ROLL_90_YAW_45, 90, 0, 45);
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test_euler(ROTATION_ROLL_90_YAW_90, 90, 0, 90);
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test_euler(ROTATION_ROLL_90_YAW_135, 90, 0, 135);
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test_euler(ROTATION_ROLL_270, 270, 0, 0);
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test_euler(ROTATION_ROLL_270_YAW_45, 270, 0, 45);
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test_euler(ROTATION_ROLL_270_YAW_90, 270, 0, 90);
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test_euler(ROTATION_ROLL_270_YAW_135, 270, 0, 135);
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test_euler(ROTATION_PITCH_90, 0, 90, 0);
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test_euler(ROTATION_PITCH_270, 0, 270, 0);
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test_euler(ROTATION_PITCH_180_YAW_90, 0, 180, 90);
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test_euler(ROTATION_PITCH_180_YAW_270, 0, 180, 270);
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test_euler(ROTATION_ROLL_90_PITCH_90, 90, 90, 0);
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test_euler(ROTATION_ROLL_180_PITCH_90,180, 90, 0);
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test_euler(ROTATION_ROLL_270_PITCH_90,270, 90, 0);
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test_euler(ROTATION_ROLL_90_PITCH_180, 90, 180, 0);
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test_euler(ROTATION_ROLL_270_PITCH_180,270,180, 0);
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test_euler(ROTATION_ROLL_90_PITCH_270, 90, 270, 0);
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test_euler(ROTATION_ROLL_180_PITCH_270,180,270, 0);
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test_euler(ROTATION_ROLL_270_PITCH_270,270,270, 0);
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test_euler(ROTATION_ROLL_90_PITCH_180_YAW_90, 90, 180, 90);
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test_euler(ROTATION_ROLL_90_YAW_270, 90, 0, 270);
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test_euler(ROTATION_YAW_293_PITCH_68_ROLL_90,90,68.8,293.3);
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}
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static bool have_rotation(const Matrix3f &m)
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{
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Matrix3f mt = m.transposed();
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for (enum Rotation r=ROTATION_NONE;
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r<ROTATION_MAX;
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r = (enum Rotation)((uint8_t)r+1)) {
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Vector3f v(1,2,3);
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Vector3f v2 = v;
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v2.rotate(r);
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v2 = mt * v2;
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if ((v2 - v).length() < 0.01f) {
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return true;
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}
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}
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return false;
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}
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static void missing_rotations(void)
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{
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hal.console->println("testing for missing rotations");
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uint16_t roll, pitch, yaw;
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for (yaw=0; yaw<360; yaw += 90)
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for (pitch=0; pitch<360; pitch += 90)
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for (roll=0; roll<360; roll += 90) {
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Matrix3f m;
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m.from_euler(ToRad(roll), ToRad(pitch), ToRad(yaw));
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if (!have_rotation(m)) {
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hal.console->printf("Missing rotation (%u, %u, %u)\n", roll, pitch, yaw);
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}
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}
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}
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/*
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* rotation tests
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*/
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void setup(void)
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{
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hal.console->println("rotation unit tests\n");
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test_rotation_accuracy();
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test_eulers();
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missing_rotations();
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hal.console->println("rotation unit tests done\n");
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}
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void loop(void) {}
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AP_HAL_MAIN();
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