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Adding debug declaration to allow imu unit tests to compile.
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1 changed files with 115 additions and 113 deletions
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/*
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/*
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* This file is part of Cleanflight.
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* This file is part of Cleanflight.
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*
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*
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* Cleanflight is free software: you can redistribute it and/or modify
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* Cleanflight 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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* 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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* 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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* (at your option) any later version.
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*
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*
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* Cleanflight is distributed in the hope that it will be useful,
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* Cleanflight 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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* 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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* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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* GNU General Public License for more details.
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* GNU General Public License for more details.
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*
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*
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* You should have received a copy of the GNU General Public License
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* You should have received a copy of the GNU General Public License
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* along with Cleanflight. If not, see <http://www.gnu.org/licenses/>.
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* along with Cleanflight. If not, see <http://www.gnu.org/licenses/>.
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*/
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*/
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#include <stdint.h>
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#include <stdint.h>
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#include <stdbool.h>
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#include <stdbool.h>
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#include <limits.h>
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#include <limits.h>
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#define BARO
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#define BARO
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#include "common/axis.h"
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#include "common/axis.h"
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#include "flight/flight.h"
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#include "flight/flight.h"
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#include "sensors/sensors.h"
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#include "sensors/sensors.h"
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#include "drivers/accgyro.h"
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#include "drivers/accgyro.h"
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#include "sensors/gyro.h"
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#include "sensors/gyro.h"
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#include "sensors/compass.h"
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#include "sensors/compass.h"
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#include "sensors/acceleration.h"
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#include "sensors/acceleration.h"
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#include "sensors/barometer.h"
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#include "sensors/barometer.h"
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#include "config/runtime_config.h"
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#include "config/runtime_config.h"
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#include "flight/mixer.h"
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#include "flight/mixer.h"
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#include "flight/imu.h"
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#include "flight/imu.h"
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#include "unittest_macros.h"
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#include "unittest_macros.h"
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#include "gtest/gtest.h"
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#include "gtest/gtest.h"
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#define DOWNWARDS_THRUST true
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#define DOWNWARDS_THRUST true
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#define UPWARDS_THRUST false
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#define UPWARDS_THRUST false
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bool isThrustFacingDownwards(rollAndPitchInclination_t *inclinations);
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bool isThrustFacingDownwards(rollAndPitchInclination_t *inclinations);
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typedef struct inclinationExpectation_s {
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typedef struct inclinationExpectation_s {
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rollAndPitchInclination_t inclination;
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rollAndPitchInclination_t inclination;
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bool expectDownwardsThrust;
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bool expectDownwardsThrust;
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} inclinationExpectation_t;
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} inclinationExpectation_t;
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TEST(FlightImuTest, IsThrustFacingDownwards)
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TEST(FlightImuTest, IsThrustFacingDownwards)
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{
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{
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// given
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// given
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inclinationExpectation_t inclinationExpectations[] = {
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inclinationExpectation_t inclinationExpectations[] = {
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{ { 0, 0 }, DOWNWARDS_THRUST },
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{ { 0, 0 }, DOWNWARDS_THRUST },
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{ { 799, 799 }, DOWNWARDS_THRUST },
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{ { 799, 799 }, DOWNWARDS_THRUST },
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{ { 800, 799 }, UPWARDS_THRUST },
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{ { 800, 799 }, UPWARDS_THRUST },
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{ { 799, 800 }, UPWARDS_THRUST },
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{ { 799, 800 }, UPWARDS_THRUST },
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{ { 800, 800 }, UPWARDS_THRUST },
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{ { 800, 800 }, UPWARDS_THRUST },
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{ { 801, 801 }, UPWARDS_THRUST },
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{ { 801, 801 }, UPWARDS_THRUST },
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{ { -799, -799 }, DOWNWARDS_THRUST },
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{ { -799, -799 }, DOWNWARDS_THRUST },
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{ { -800, -799 }, UPWARDS_THRUST },
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{ { -800, -799 }, UPWARDS_THRUST },
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{ { -799, -800 }, UPWARDS_THRUST },
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{ { -799, -800 }, UPWARDS_THRUST },
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{ { -800, -800 }, UPWARDS_THRUST },
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{ { -800, -800 }, UPWARDS_THRUST },
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{ { -801, -801 }, UPWARDS_THRUST }
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{ { -801, -801 }, UPWARDS_THRUST }
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};
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};
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uint8_t testIterationCount = sizeof(inclinationExpectations) / sizeof(inclinationExpectation_t);
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uint8_t testIterationCount = sizeof(inclinationExpectations) / sizeof(inclinationExpectation_t);
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// expect
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// expect
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for (uint8_t index = 0; index < testIterationCount; index ++) {
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for (uint8_t index = 0; index < testIterationCount; index ++) {
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inclinationExpectation_t *angleInclinationExpectation = &inclinationExpectations[index];
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inclinationExpectation_t *angleInclinationExpectation = &inclinationExpectations[index];
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printf("iteration: %d\n", index);
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printf("iteration: %d\n", index);
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bool result = isThrustFacingDownwards(&angleInclinationExpectation->inclination);
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bool result = isThrustFacingDownwards(&angleInclinationExpectation->inclination);
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EXPECT_EQ(angleInclinationExpectation->expectDownwardsThrust, result);
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EXPECT_EQ(angleInclinationExpectation->expectDownwardsThrust, result);
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}
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}
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}
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}
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// STUBS
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// STUBS
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uint16_t acc_1G;
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uint16_t acc_1G;
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int16_t heading;
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int16_t heading;
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flags_t f;
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flags_t f;
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gyro_t gyro;
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gyro_t gyro;
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int16_t magADC[XYZ_AXIS_COUNT];
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int16_t magADC[XYZ_AXIS_COUNT];
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int32_t BaroAlt;
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int32_t BaroAlt;
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int16_t debug[4];
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void gyroGetADC(void) {};
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bool sensors(uint32_t mask)
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{
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void gyroGetADC(void) {};
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UNUSED(mask);
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bool sensors(uint32_t mask)
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return false;
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{
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};
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UNUSED(mask);
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void updateAccelerationReadings(rollAndPitchTrims_t *rollAndPitchTrims)
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return false;
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{
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};
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UNUSED(rollAndPitchTrims);
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void updateAccelerationReadings(rollAndPitchTrims_t *rollAndPitchTrims)
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}
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{
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UNUSED(rollAndPitchTrims);
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uint32_t micros(void) { return 0; }
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}
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bool isBaroCalibrationComplete(void) { return true; }
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void performBaroCalibrationCycle(void) {}
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uint32_t micros(void) { return 0; }
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int32_t baroCalculateAltitude(void) { return 0; }
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bool isBaroCalibrationComplete(void) { return true; }
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int constrain(int amt, int low, int high)
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void performBaroCalibrationCycle(void) {}
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{
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int32_t baroCalculateAltitude(void) { return 0; }
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UNUSED(amt);
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int constrain(int amt, int low, int high)
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UNUSED(low);
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{
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UNUSED(high);
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UNUSED(amt);
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return 0;
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UNUSED(low);
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}
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UNUSED(high);
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return 0;
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}
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