mirror of
https://github.com/betaflight/betaflight.git
synced 2025-07-13 11:29:58 +03:00
* 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
216 lines
7.8 KiB
C++
216 lines
7.8 KiB
C++
/*
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* This file is part of Cleanflight.
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*
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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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* 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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*
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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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* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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* GNU General Public License for more details.
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*
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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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*/
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#include <stdint.h>
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extern "C" {
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#include "blackbox/blackbox.h"
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#include "build/debug.h"
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#include "common/maths.h"
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#include "common/streambuf.h"
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#include "config/feature.h"
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#include "config/config.h"
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#include "fc/controlrate_profile.h"
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#include "fc/core.h"
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#include "fc/rc_controls.h"
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#include "fc/rc_modes.h"
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#include "fc/runtime_config.h"
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#include "flight/failsafe.h"
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#include "flight/imu.h"
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#include "flight/mixer.h"
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#include "flight/pid.h"
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#include "flight/servos.h"
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#include "flight/gps_rescue.h"
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#include "io/beeper.h"
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#include "io/gps.h"
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#include "io/vtx.h"
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#include "pg/gps_rescue.h"
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#include "pg/motor.h"
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#include "pg/pg.h"
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#include "pg/pg_ids.h"
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#include "pg/rx.h"
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#include "rx/rx.h"
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#include "scheduler/scheduler.h"
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#include "sensors/acceleration.h"
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#include "sensors/gyro.h"
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#include "telemetry/telemetry.h"
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vtxSettingsConfig_t vtxGetSettings(void);
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PG_REGISTER(accelerometerConfig_t, accelerometerConfig, PG_ACCELEROMETER_CONFIG, 0);
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PG_REGISTER(blackboxConfig_t, blackboxConfig, PG_BLACKBOX_CONFIG, 0);
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PG_REGISTER(gyroConfig_t, gyroConfig, PG_GYRO_CONFIG, 0);
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PG_REGISTER(mixerConfig_t, mixerConfig, PG_MIXER_CONFIG, 0);
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PG_REGISTER(pidConfig_t, pidConfig, PG_PID_CONFIG, 0);
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PG_REGISTER(rxConfig_t, rxConfig, PG_RX_CONFIG, 0);
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PG_REGISTER(servoConfig_t, servoConfig, PG_SERVO_CONFIG, 0);
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PG_REGISTER(systemConfig_t, systemConfig, PG_SYSTEM_CONFIG, 0);
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PG_REGISTER(telemetryConfig_t, telemetryConfig, PG_TELEMETRY_CONFIG, 0);
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PG_REGISTER(failsafeConfig_t, failsafeConfig, PG_FAILSAFE_CONFIG, 0);
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PG_REGISTER(motorConfig_t, motorConfig, PG_MOTOR_CONFIG, 0);
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PG_REGISTER(imuConfig_t, imuConfig, PG_IMU_CONFIG, 0);
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PG_REGISTER(gpsRescueConfig_t, gpsRescueConfig, PG_GPS_CONFIG, 0);
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extern float rcCommand[4];
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float rcData[MAX_SUPPORTED_RC_CHANNEL_COUNT];
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uint16_t averageSystemLoadPercent = 0;
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uint8_t cliMode = 0;
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uint8_t debugMode = 0;
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int16_t debug[DEBUG16_VALUE_COUNT];
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pidProfile_t *currentPidProfile;
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controlRateConfig_t *currentControlRateProfile;
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attitudeEulerAngles_t attitude;
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gpsSolutionData_t gpsSol;
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uint32_t targetPidLooptime;
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bool cmsInMenu = false;
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float axisPID_P[3], axisPID_I[3], axisPID_D[3], axisPIDSum[3];
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rxRuntimeState_t rxRuntimeState = {};
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acc_t acc;
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}
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uint32_t simulationFeatureFlags = 0;
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uint32_t simulationTime = 0;
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bool gyroCalibDone = false;
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bool simulationHaveRx = false;
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#include "gtest/gtest.h"
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TEST(VtxTest, PitMode)
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{
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// given
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modeActivationConditionsMutable(0)->auxChannelIndex = 0;
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modeActivationConditionsMutable(0)->modeId = BOXVTXPITMODE;
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modeActivationConditionsMutable(0)->range.startStep = CHANNEL_VALUE_TO_STEP(1750);
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modeActivationConditionsMutable(0)->range.endStep = CHANNEL_VALUE_TO_STEP(CHANNEL_RANGE_MAX);
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analyzeModeActivationConditions();
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// and
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vtxSettingsConfigMutable()->band = 0;
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vtxSettingsConfigMutable()->freq = 5800;
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vtxSettingsConfigMutable()->pitModeFreq = 5300;
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// expect
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EXPECT_EQ(5800, vtxGetSettings().freq);
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// and
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// enable vtx pit mode
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rcData[AUX1] = 1800;
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// when
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updateActivatedModes();
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// expect
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EXPECT_TRUE(IS_RC_MODE_ACTIVE(BOXVTXPITMODE));
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EXPECT_EQ(5300, vtxGetSettings().freq);
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}
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// STUBS
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extern "C" {
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uint8_t activePidLoopDenom = 1;
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uint32_t micros(void) { return simulationTime; }
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uint32_t millis(void) { return micros() / 1000; }
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bool isRxReceivingSignal(void) { return simulationHaveRx; }
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bool featureIsEnabled(uint32_t f) { return simulationFeatureFlags & f; }
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void warningLedFlash(void) {}
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void warningLedDisable(void) {}
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void warningLedUpdate(void) {}
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void beeper(beeperMode_e) {}
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void beeperConfirmationBeeps(uint8_t) {}
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void beeperWarningBeeps(uint8_t) {}
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void beeperSilence(void) {}
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void systemBeep(bool) {}
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void saveConfigAndNotify(void) {}
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void blackboxFinish(void) {}
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bool accIsCalibrationComplete(void) { return true; }
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bool accHasBeenCalibrated(void) { return true; }
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bool baroIsCalibrated(void) { return true; }
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bool gyroIsCalibrationComplete(void) { return gyroCalibDone; }
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void gyroStartCalibration(bool) {}
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bool isFirstArmingGyroCalibrationRunning(void) { return false; }
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void pidController(const pidProfile_t *, timeUs_t) {}
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void pidStabilisationState(pidStabilisationState_e) {}
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void mixTable(timeUs_t) {};
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void writeMotors(void) {};
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void writeServos(void) {};
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bool calculateRxChannelsAndUpdateFailsafe(timeUs_t) { return true; }
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bool isMixerUsingServos(void) { return false; }
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void gyroUpdate() {}
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timeDelta_t getTaskDeltaTimeUs(taskId_e) { return 0; }
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void updateRSSI(timeUs_t) {}
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bool failsafeIsMonitoring(void) { return false; }
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void failsafeStartMonitoring(void) {}
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void failsafeUpdateState(void) {}
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bool failsafeIsActive(void) { return false; }
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bool rxAreFlightChannelsValid(void) { return false; }
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bool failsafeIsReceivingRxData(void) { return false; }
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void pidResetIterm(void) {}
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void updateAdjustmentStates(void) {}
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void processRcAdjustments(controlRateConfig_t *) {}
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void updateGpsWaypointsAndMode(void) {}
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void mspSerialReleaseSharedTelemetryPorts(void) {}
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void telemetryCheckState(void) {}
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void mspSerialAllocatePorts(void) {}
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void gyroReadTemperature(void) {}
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void updateRcCommands(void) {}
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void applyAltHold(void) {}
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void resetYawAxis(void) {}
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int16_t calculateThrottleAngleCorrection(uint8_t) { return 0; }
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void processRcCommand(void) {}
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void updateGpsStateForHomeAndHoldMode(void) {}
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void blackboxUpdate(timeUs_t) {}
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void transponderUpdate(timeUs_t) {}
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void GPS_reset_home_position(void) {}
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void accStartCalibration(void) {}
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void baroSetGroundLevel(void) {}
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void changePidProfile(uint8_t) {}
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void changeControlRateProfile(uint8_t) {}
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void dashboardEnablePageCycling(void) {}
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void dashboardDisablePageCycling(void) {}
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bool imuQuaternionHeadfreeOffsetSet(void) { return true; }
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void rescheduleTask(taskId_e, timeDelta_t) {}
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bool usbCableIsInserted(void) { return false; }
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bool usbVcpIsConnected(void) { return false; }
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void pidSetAntiGravityState(bool newState) { UNUSED(newState); }
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void osdSuppressStats(bool) {}
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void pidSetItermReset(bool) {}
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void applyAccelerometerTrimsDelta(rollAndPitchTrims_t*) {}
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bool isFixedWing(void) { return false; }
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void compassStartCalibration(void) {}
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bool compassIsCalibrationComplete(void) { return true; }
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bool isUpright(void) { return true; }
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void blackboxLogEvent(FlightLogEvent, union flightLogEventData_u *) {};
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void gyroFiltering(timeUs_t) {};
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timeDelta_t rxGetFrameDelta() { return 0; }
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void updateRcRefreshRate(timeUs_t) {};
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uint16_t getAverageSystemLoadPercent(void) { return 0; }
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bool isMotorProtocolEnabled(void) { return false; }
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void pinioBoxTaskControl(void) {}
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void sbufWriteU8(sbuf_t *, uint8_t) {}
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void sbufWriteU16(sbuf_t *, uint16_t) {}
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void sbufWriteU32(sbuf_t *, uint32_t) {}
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void schedulerSetNextStateTime(timeDelta_t) {}
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bool crashFlipSuccessful(void) {return false; }
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}
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