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betaflight/src/test/unit/vtx_unittest.cc
ctzsnooze 7156dc84a3
Update turtle / crashflip mode (#13905)
* stop motors after 90 degrees of rotation and with max rate

* handle no accelerometer data

* improve check for acc, although seems to be OK without it

* disable all attenuation if rate is set to zero

* refactoring thanks Karate

* use sensors.h

* remove unnecessary arming check

* exit crashFlip immediately switch is reverted if throttle is zero

* add Crashflip Rate to OSD

* Revert unnecessary changes in crashflip core.c code

and clarify comments about crashflip switch

* update / minimise comments, thanks Karate

* ensure all names say `crashflip` consistently

* Undo quick re-arm because motrors were not reversed

* fix issue with reversed motors, we must disarm

* ignore yaw rotation and set gyro limit to 1900 deg/s

* default attenuation to off (crashflip_rate = 0)

* refactoring, increase rate limit to allow stronger inhibition

* enable in race_pro mode

* don't attenuate on attitude until a significant change occurs

* no attenuation for small changes

* Updates from review by PL

* remove whitespace

* refactor motorOutput, update comments, renaming variables

thanks PL

* changes from review PL

* only permit fast re-arm if crashflip rate set and crashflip was successful

* properly exit turtle mode

* add crashFlipSuccessful to unit test extern c

* small updates from review

* improved crashflip switch handling

* remove unnecessary motors normal check
2024-10-05 07:58:33 +10:00

216 lines
7.8 KiB
C++

/*
* This file is part of Cleanflight.
*
* Cleanflight is free software: you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation, either version 3 of the License, or
* (at your option) any later version.
*
* Cleanflight is distributed in the hope that it will be useful,
* but WITHOUT ANY WARRANTY; without even the implied warranty of
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
* GNU General Public License for more details.
*
* You should have received a copy of the GNU General Public License
* along with Cleanflight. If not, see <http://www.gnu.org/licenses/>.
*/
#include <stdint.h>
extern "C" {
#include "blackbox/blackbox.h"
#include "build/debug.h"
#include "common/maths.h"
#include "common/streambuf.h"
#include "config/feature.h"
#include "config/config.h"
#include "fc/controlrate_profile.h"
#include "fc/core.h"
#include "fc/rc_controls.h"
#include "fc/rc_modes.h"
#include "fc/runtime_config.h"
#include "flight/failsafe.h"
#include "flight/imu.h"
#include "flight/mixer.h"
#include "flight/pid.h"
#include "flight/servos.h"
#include "flight/gps_rescue.h"
#include "io/beeper.h"
#include "io/gps.h"
#include "io/vtx.h"
#include "pg/gps_rescue.h"
#include "pg/motor.h"
#include "pg/pg.h"
#include "pg/pg_ids.h"
#include "pg/rx.h"
#include "rx/rx.h"
#include "scheduler/scheduler.h"
#include "sensors/acceleration.h"
#include "sensors/gyro.h"
#include "telemetry/telemetry.h"
vtxSettingsConfig_t vtxGetSettings(void);
PG_REGISTER(accelerometerConfig_t, accelerometerConfig, PG_ACCELEROMETER_CONFIG, 0);
PG_REGISTER(blackboxConfig_t, blackboxConfig, PG_BLACKBOX_CONFIG, 0);
PG_REGISTER(gyroConfig_t, gyroConfig, PG_GYRO_CONFIG, 0);
PG_REGISTER(mixerConfig_t, mixerConfig, PG_MIXER_CONFIG, 0);
PG_REGISTER(pidConfig_t, pidConfig, PG_PID_CONFIG, 0);
PG_REGISTER(rxConfig_t, rxConfig, PG_RX_CONFIG, 0);
PG_REGISTER(servoConfig_t, servoConfig, PG_SERVO_CONFIG, 0);
PG_REGISTER(systemConfig_t, systemConfig, PG_SYSTEM_CONFIG, 0);
PG_REGISTER(telemetryConfig_t, telemetryConfig, PG_TELEMETRY_CONFIG, 0);
PG_REGISTER(failsafeConfig_t, failsafeConfig, PG_FAILSAFE_CONFIG, 0);
PG_REGISTER(motorConfig_t, motorConfig, PG_MOTOR_CONFIG, 0);
PG_REGISTER(imuConfig_t, imuConfig, PG_IMU_CONFIG, 0);
PG_REGISTER(gpsRescueConfig_t, gpsRescueConfig, PG_GPS_CONFIG, 0);
extern float rcCommand[4];
float rcData[MAX_SUPPORTED_RC_CHANNEL_COUNT];
uint16_t averageSystemLoadPercent = 0;
uint8_t cliMode = 0;
uint8_t debugMode = 0;
int16_t debug[DEBUG16_VALUE_COUNT];
pidProfile_t *currentPidProfile;
controlRateConfig_t *currentControlRateProfile;
attitudeEulerAngles_t attitude;
gpsSolutionData_t gpsSol;
uint32_t targetPidLooptime;
bool cmsInMenu = false;
float axisPID_P[3], axisPID_I[3], axisPID_D[3], axisPIDSum[3];
rxRuntimeState_t rxRuntimeState = {};
acc_t acc;
}
uint32_t simulationFeatureFlags = 0;
uint32_t simulationTime = 0;
bool gyroCalibDone = false;
bool simulationHaveRx = false;
#include "gtest/gtest.h"
TEST(VtxTest, PitMode)
{
// given
modeActivationConditionsMutable(0)->auxChannelIndex = 0;
modeActivationConditionsMutable(0)->modeId = BOXVTXPITMODE;
modeActivationConditionsMutable(0)->range.startStep = CHANNEL_VALUE_TO_STEP(1750);
modeActivationConditionsMutable(0)->range.endStep = CHANNEL_VALUE_TO_STEP(CHANNEL_RANGE_MAX);
analyzeModeActivationConditions();
// and
vtxSettingsConfigMutable()->band = 0;
vtxSettingsConfigMutable()->freq = 5800;
vtxSettingsConfigMutable()->pitModeFreq = 5300;
// expect
EXPECT_EQ(5800, vtxGetSettings().freq);
// and
// enable vtx pit mode
rcData[AUX1] = 1800;
// when
updateActivatedModes();
// expect
EXPECT_TRUE(IS_RC_MODE_ACTIVE(BOXVTXPITMODE));
EXPECT_EQ(5300, vtxGetSettings().freq);
}
// STUBS
extern "C" {
uint8_t activePidLoopDenom = 1;
uint32_t micros(void) { return simulationTime; }
uint32_t millis(void) { return micros() / 1000; }
bool isRxReceivingSignal(void) { return simulationHaveRx; }
bool featureIsEnabled(uint32_t f) { return simulationFeatureFlags & f; }
void warningLedFlash(void) {}
void warningLedDisable(void) {}
void warningLedUpdate(void) {}
void beeper(beeperMode_e) {}
void beeperConfirmationBeeps(uint8_t) {}
void beeperWarningBeeps(uint8_t) {}
void beeperSilence(void) {}
void systemBeep(bool) {}
void saveConfigAndNotify(void) {}
void blackboxFinish(void) {}
bool accIsCalibrationComplete(void) { return true; }
bool accHasBeenCalibrated(void) { return true; }
bool baroIsCalibrated(void) { return true; }
bool gyroIsCalibrationComplete(void) { return gyroCalibDone; }
void gyroStartCalibration(bool) {}
bool isFirstArmingGyroCalibrationRunning(void) { return false; }
void pidController(const pidProfile_t *, timeUs_t) {}
void pidStabilisationState(pidStabilisationState_e) {}
void mixTable(timeUs_t) {};
void writeMotors(void) {};
void writeServos(void) {};
bool calculateRxChannelsAndUpdateFailsafe(timeUs_t) { return true; }
bool isMixerUsingServos(void) { return false; }
void gyroUpdate() {}
timeDelta_t getTaskDeltaTimeUs(taskId_e) { return 0; }
void updateRSSI(timeUs_t) {}
bool failsafeIsMonitoring(void) { return false; }
void failsafeStartMonitoring(void) {}
void failsafeUpdateState(void) {}
bool failsafeIsActive(void) { return false; }
bool rxAreFlightChannelsValid(void) { return false; }
bool failsafeIsReceivingRxData(void) { return false; }
void pidResetIterm(void) {}
void updateAdjustmentStates(void) {}
void processRcAdjustments(controlRateConfig_t *) {}
void updateGpsWaypointsAndMode(void) {}
void mspSerialReleaseSharedTelemetryPorts(void) {}
void telemetryCheckState(void) {}
void mspSerialAllocatePorts(void) {}
void gyroReadTemperature(void) {}
void updateRcCommands(void) {}
void applyAltHold(void) {}
void resetYawAxis(void) {}
int16_t calculateThrottleAngleCorrection(uint8_t) { return 0; }
void processRcCommand(void) {}
void updateGpsStateForHomeAndHoldMode(void) {}
void blackboxUpdate(timeUs_t) {}
void transponderUpdate(timeUs_t) {}
void GPS_reset_home_position(void) {}
void accStartCalibration(void) {}
void baroSetGroundLevel(void) {}
void changePidProfile(uint8_t) {}
void changeControlRateProfile(uint8_t) {}
void dashboardEnablePageCycling(void) {}
void dashboardDisablePageCycling(void) {}
bool imuQuaternionHeadfreeOffsetSet(void) { return true; }
void rescheduleTask(taskId_e, timeDelta_t) {}
bool usbCableIsInserted(void) { return false; }
bool usbVcpIsConnected(void) { return false; }
void pidSetAntiGravityState(bool newState) { UNUSED(newState); }
void osdSuppressStats(bool) {}
void pidSetItermReset(bool) {}
void applyAccelerometerTrimsDelta(rollAndPitchTrims_t*) {}
bool isFixedWing(void) { return false; }
void compassStartCalibration(void) {}
bool compassIsCalibrationComplete(void) { return true; }
bool isUpright(void) { return true; }
void blackboxLogEvent(FlightLogEvent, union flightLogEventData_u *) {};
void gyroFiltering(timeUs_t) {};
timeDelta_t rxGetFrameDelta() { return 0; }
void updateRcRefreshRate(timeUs_t) {};
uint16_t getAverageSystemLoadPercent(void) { return 0; }
bool isMotorProtocolEnabled(void) { return false; }
void pinioBoxTaskControl(void) {}
void sbufWriteU8(sbuf_t *, uint8_t) {}
void sbufWriteU16(sbuf_t *, uint16_t) {}
void sbufWriteU32(sbuf_t *, uint32_t) {}
void schedulerSetNextStateTime(timeDelta_t) {}
bool crashFlipSuccessful(void) {return false; }
}