Exemplo n.º 1
0
void annexCode(void)
{

    int32_t throttleValue;

    // Compute ROLL PITCH and YAW command
    rcCommand[ROLL] = getAxisRcCommand(rcData[ROLL], currentControlRateProfile->rcExpo8, currentProfile->rcControlsConfig.deadband);
    rcCommand[PITCH] = getAxisRcCommand(rcData[PITCH], currentControlRateProfile->rcExpo8, currentProfile->rcControlsConfig.deadband);
    rcCommand[YAW] = -getAxisRcCommand(rcData[YAW], currentControlRateProfile->rcYawExpo8, currentProfile->rcControlsConfig.yaw_deadband);

    //Compute THROTTLE command
    throttleValue = constrain(rcData[THROTTLE], masterConfig.rxConfig.mincheck, PWM_RANGE_MAX);
    throttleValue = (uint32_t)(throttleValue - masterConfig.rxConfig.mincheck) * PWM_RANGE_MIN / (PWM_RANGE_MAX - masterConfig.rxConfig.mincheck);       // [MINCHECK;2000] -> [0;1000]
    rcCommand[THROTTLE] = rcLookupThrottle(throttleValue);

    if (FLIGHT_MODE(HEADFREE_MODE)) {
        const float radDiff = degreesToRadians(DECIDEGREES_TO_DEGREES(attitude.values.yaw) - headFreeModeHold);
        const float cosDiff = cos_approx(radDiff);
        const float sinDiff = sin_approx(radDiff);
        const int16_t rcCommand_PITCH = rcCommand[PITCH] * cosDiff + rcCommand[ROLL] * sinDiff;
        rcCommand[ROLL] = rcCommand[ROLL] * cosDiff - rcCommand[PITCH] * sinDiff;
        rcCommand[PITCH] = rcCommand_PITCH;
    }

    if (ARMING_FLAG(ARMED)) {
        LED0_ON;
    } else {
        if (IS_RC_MODE_ACTIVE(BOXARM) == 0) {
            ENABLE_ARMING_FLAG(OK_TO_ARM);
        }

        if (!STATE(SMALL_ANGLE)) {
            DISABLE_ARMING_FLAG(OK_TO_ARM);
        }

        if (isCalibrating() || isSystemOverloaded()) {
            warningLedFlash();
            DISABLE_ARMING_FLAG(OK_TO_ARM);
        }

#if defined(NAV)
        if (naivationBlockArming()) {
            DISABLE_ARMING_FLAG(OK_TO_ARM);
        }
#endif

        if (ARMING_FLAG(OK_TO_ARM)) {
            warningLedDisable();
        } else {
            warningLedFlash();
        }

        warningLedUpdate();
    }

    // Read out gyro temperature. can use it for something somewhere. maybe get MCU temperature instead? lots of fun possibilities.
    if (gyro.temperature)
        gyro.temperature(&telemTemperature1);
}
Exemplo n.º 2
0
armingPreventedReason_e getArmingPreventionBlinkMask(void)
{
    if (isCalibrating()) {
        return ARM_PREV_CALIB;
    }
    if (rcModeIsActive(BOXFAILSAFE) || failsafePhase() == FAILSAFE_LANDED) {
        return ARM_PREV_FAILSAFE;
    }
    if (!imuIsAircraftArmable(armingConfig()->max_arm_angle)) {
        return ARM_PREV_ANGLE;
    }
    if (cliMode) {
        return ARM_PREV_CLI;
    }
    if (isSystemOverloaded()) {
        return ARM_PREV_OVERLOAD;
    }
    return ARM_PREV_NONE;
}
Exemplo n.º 3
0
void annexCode(void)
{
    if (FLIGHT_MODE(HEADFREE_MODE)) {
        float radDiff = degreesToRadians(DECIDEGREES_TO_DEGREES(attitude.values.yaw) - headFreeModeHold);
        float cosDiff = cos_approx(radDiff);
        float sinDiff = sin_approx(radDiff);
        int16_t rcCommand_PITCH = rcCommand[PITCH] * cosDiff + rcCommand[ROLL] * sinDiff;
        rcCommand[ROLL] = rcCommand[ROLL] * cosDiff - rcCommand[PITCH] * sinDiff;
        rcCommand[PITCH] = rcCommand_PITCH;
    }

    if (ARMING_FLAG(ARMED)) {
        LED0_ON;
    } else {
        if (rcModeIsActive(BOXARM) == 0) {
            ENABLE_ARMING_FLAG(OK_TO_ARM);
        }

        if (!imuIsAircraftArmable(armingConfig()->max_arm_angle)) {
            DISABLE_ARMING_FLAG(OK_TO_ARM);
        }

        if (isCalibrating() || isSystemOverloaded()) {
            warningLedFlash();
            DISABLE_ARMING_FLAG(OK_TO_ARM);
        } else {
            if (ARMING_FLAG(OK_TO_ARM)) {
                warningLedDisable();
            } else {
                warningLedFlash();
            }
        }

        warningLedUpdate();
    }

    // Read out gyro temperature. can use it for something somewhere. maybe get MCU temperature instead? lots of fun possibilities.
    if (gyro.temperature)
        gyro.temperature(&telemTemperature1);
}
Exemplo n.º 4
0
static void updateLEDs(void)
{
    if (ARMING_FLAG(ARMED)) {
        LED0_ON;
    } else {
        if (rcModeIsActive(BOXARM) == 0) {
            ENABLE_ARMING_FLAG(OK_TO_ARM);
        }

        if (!imuIsAircraftArmable(armingConfig()->max_arm_angle)) {
            DISABLE_ARMING_FLAG(OK_TO_ARM);
        }

        if (isCalibrating() || isSystemOverloaded()) {
            DISABLE_ARMING_FLAG(OK_TO_ARM);
        }

        uint32_t nextBlinkMask = getArmingPreventionBlinkMask();
        warningLedSetBlinkMask(nextBlinkMask);
        warningLedUpdate();
    }
}
Exemplo n.º 5
0
void annexCode(void)
{
    int32_t tmp, tmp2;
    tmp = constrain(rcData[THROTTLE], rxConfig()->mincheck, PWM_RANGE_MAX);
    tmp = (uint32_t)(tmp - rxConfig()->mincheck) * PWM_RANGE_MIN / (PWM_RANGE_MAX - rxConfig()->mincheck);       // [MINCHECK;2000] -> [0;1000]
    tmp2 = tmp / 100;
    rcCommand[THROTTLE] = lookupThrottleRC[tmp2] + (tmp - tmp2 * 100) * (lookupThrottleRC[tmp2 + 1] - lookupThrottleRC[tmp2]) / 100;    // [0;1000] -> expo -> [MINTHROTTLE;MAXTHROTTLE]
    
    if (ARMING_FLAG(ARMED)) {
        LED0_ON;
    } else {
        if (rcModeIsActive(BOXARM) == 0) {
            ENABLE_ARMING_FLAG(OK_TO_ARM);
        }

        if (!imuIsAircraftArmable(armingConfig()->max_arm_angle)) {
            DISABLE_ARMING_FLAG(OK_TO_ARM);
        }

        if (isCalibrating() || isSystemOverloaded()) {
            warningLedFlash();
            DISABLE_ARMING_FLAG(OK_TO_ARM);
        } else {
            if (ARMING_FLAG(OK_TO_ARM)) {
                warningLedDisable();
            } else {
                warningLedFlash();
            }
        }

        warningLedUpdate();
    }

    // Read out gyro temperature. can use it for something somewhere. maybe get MCU temperature instead? lots of fun possibilities.
    if (gyro.temperature)
        gyro.temperature(&telemTemperature1);
}
Exemplo n.º 6
0
Arquivo: mw.c Projeto: risnandar/inav
void annexCode(void)
{
    int32_t tmp;

    for (int axis = 0; axis < 3; axis++) {
        tmp = MIN(ABS(rcData[axis] - masterConfig.rxConfig.midrc), 500);
        if (axis == ROLL || axis == PITCH) {
            if (currentProfile->rcControlsConfig.deadband) {
                if (tmp > currentProfile->rcControlsConfig.deadband) {
                    tmp -= currentProfile->rcControlsConfig.deadband;
                } else {
                    tmp = 0;
                }
            }
            rcCommand[axis] = rcLookupPitchRoll(tmp);
        } else if (axis == YAW) {
            if (currentProfile->rcControlsConfig.yaw_deadband) {
                if (tmp > currentProfile->rcControlsConfig.yaw_deadband) {
                    tmp -= currentProfile->rcControlsConfig.yaw_deadband;
                } else {
                    tmp = 0;
                }
            }
            rcCommand[axis] = rcLookupYaw(tmp) * -1;
        }

        if (rcData[axis] < masterConfig.rxConfig.midrc) {
            rcCommand[axis] = -rcCommand[axis];
        }
    }

    tmp = constrain(rcData[THROTTLE], masterConfig.rxConfig.mincheck, PWM_RANGE_MAX);
    tmp = (uint32_t)(tmp - masterConfig.rxConfig.mincheck) * PWM_RANGE_MIN / (PWM_RANGE_MAX - masterConfig.rxConfig.mincheck);       // [MINCHECK;2000] -> [0;1000]
    rcCommand[THROTTLE] = rcLookupThrottle(tmp);

    if (FLIGHT_MODE(HEADFREE_MODE)) {
        const float radDiff = degreesToRadians(DECIDEGREES_TO_DEGREES(attitude.values.yaw) - headFreeModeHold);
        const float cosDiff = cos_approx(radDiff);
        const float sinDiff = sin_approx(radDiff);
        const int16_t rcCommand_PITCH = rcCommand[PITCH] * cosDiff + rcCommand[ROLL] * sinDiff;
        rcCommand[ROLL] = rcCommand[ROLL] * cosDiff - rcCommand[PITCH] * sinDiff;
        rcCommand[PITCH] = rcCommand_PITCH;
    }

    if (ARMING_FLAG(ARMED)) {
        LED0_ON;
    } else {
        if (IS_RC_MODE_ACTIVE(BOXARM) == 0) {
            ENABLE_ARMING_FLAG(OK_TO_ARM);
        }

        if (!STATE(SMALL_ANGLE)) {
            DISABLE_ARMING_FLAG(OK_TO_ARM);
        }

        if (isCalibrating() || isSystemOverloaded()) {
            warningLedFlash();
            DISABLE_ARMING_FLAG(OK_TO_ARM);
        }

#if defined(NAV)
        if (naivationBlockArming()) {
            DISABLE_ARMING_FLAG(OK_TO_ARM);
        }
#endif

        if (ARMING_FLAG(OK_TO_ARM)) {
            warningLedDisable();
        } else {
            warningLedFlash();
        }

        warningLedUpdate();
    }

    // Read out gyro temperature. can use it for something somewhere. maybe get MCU temperature instead? lots of fun possibilities.
    if (gyro.temperature)
        gyro.temperature(&telemTemperature1);
}
Exemplo n.º 7
0
void annexCode(void)
{
    int32_t tmp, tmp2;
    int32_t axis, prop1 = 0, prop2;

    // PITCH & ROLL only dynamic PID adjustment,  depending on throttle value
    if (rcData[THROTTLE] < currentControlRateProfile->tpa_breakpoint) {
        prop2 = 100;
    } else {
        if (rcData[THROTTLE] < 2000) {
            prop2 = 100 - (uint16_t)currentControlRateProfile->dynThrPID * (rcData[THROTTLE] - currentControlRateProfile->tpa_breakpoint) / (2000 - currentControlRateProfile->tpa_breakpoint);
        } else {
            prop2 = 100 - currentControlRateProfile->dynThrPID;
        }
    }

    for (axis = 0; axis < 3; axis++) {
        tmp = MIN(ABS(rcData[axis] - rxConfig()->midrc), 500);
        if (axis == ROLL || axis == PITCH) {
            if (rcControlsConfig()->deadband) {
                if (tmp > rcControlsConfig()->deadband) {
                    tmp -= rcControlsConfig()->deadband;
                } else {
                    tmp = 0;
                }
            }

            tmp2 = tmp / 100;
            rcCommand[axis] = lookupPitchRollRC[tmp2] + (tmp - tmp2 * 100) * (lookupPitchRollRC[tmp2 + 1] - lookupPitchRollRC[tmp2]) / 100;
            prop1 = 100 - (uint16_t)currentControlRateProfile->rates[axis] * tmp / 500;
            prop1 = (uint16_t)prop1 * prop2 / 100;
        } else if (axis == YAW) {
            if (rcControlsConfig()->yaw_deadband) {
                if (tmp > rcControlsConfig()->yaw_deadband) {
                    tmp -= rcControlsConfig()->yaw_deadband;
                } else {
                    tmp = 0;
                }
            }
            tmp2 = tmp / 100;
            rcCommand[axis] = (lookupYawRC[tmp2] + (tmp - tmp2 * 100) * (lookupYawRC[tmp2 + 1] - lookupYawRC[tmp2]) / 100) * -rcControlsConfig()->yaw_control_direction;
            prop1 = 100 - (uint16_t)currentControlRateProfile->rates[axis] * ABS(tmp) / 500;
        }
        // FIXME axis indexes into pids.  use something like lookupPidIndex(rc_alias_e alias) to reduce coupling.
        dynP8[axis] = (uint16_t)pidProfile()->P8[axis] * prop1 / 100;
        dynI8[axis] = (uint16_t)pidProfile()->I8[axis] * prop1 / 100;
        dynD8[axis] = (uint16_t)pidProfile()->D8[axis] * prop1 / 100;

        // non coupled PID reduction scaler used in PID controller 1 and PID controller 2. YAW TPA disabled. 100 means 100% of the pids
        if (axis == YAW) {
            PIDweight[axis] = 100;
        }
        else {
            PIDweight[axis] = prop2;
        }

        if (rcData[axis] < rxConfig()->midrc)
            rcCommand[axis] = -rcCommand[axis];
    }

    tmp = constrain(rcData[THROTTLE], rxConfig()->mincheck, PWM_RANGE_MAX);
    tmp = (uint32_t)(tmp - rxConfig()->mincheck) * PWM_RANGE_MIN / (PWM_RANGE_MAX - rxConfig()->mincheck);       // [MINCHECK;2000] -> [0;1000]
    tmp2 = tmp / 100;
    rcCommand[THROTTLE] = lookupThrottleRC[tmp2] + (tmp - tmp2 * 100) * (lookupThrottleRC[tmp2 + 1] - lookupThrottleRC[tmp2]) / 100;    // [0;1000] -> expo -> [MINTHROTTLE;MAXTHROTTLE]

    if (FLIGHT_MODE(HEADFREE_MODE)) {
        float radDiff = degreesToRadians(DECIDEGREES_TO_DEGREES(attitude.values.yaw) - headFreeModeHold);
        float cosDiff = cos_approx(radDiff);
        float sinDiff = sin_approx(radDiff);
        int16_t rcCommand_PITCH = rcCommand[PITCH] * cosDiff + rcCommand[ROLL] * sinDiff;
        rcCommand[ROLL] = rcCommand[ROLL] * cosDiff - rcCommand[PITCH] * sinDiff;
        rcCommand[PITCH] = rcCommand_PITCH;
    }

    if (ARMING_FLAG(ARMED)) {
        LED0_ON;
    } else {
        if (IS_RC_MODE_ACTIVE(BOXARM) == 0) {
            ENABLE_ARMING_FLAG(OK_TO_ARM);
        }

        if (!imuIsAircraftArmable(armingConfig()->max_arm_angle)) {
            DISABLE_ARMING_FLAG(OK_TO_ARM);
            debug[3] = ARMING_FLAG(OK_TO_ARM);
        }

        if (isCalibrating() || isSystemOverloaded()) {
            warningLedFlash();
            DISABLE_ARMING_FLAG(OK_TO_ARM);
        } else {
            if (ARMING_FLAG(OK_TO_ARM)) {
                warningLedDisable();
            } else {
                warningLedFlash();
            }
        }

        debug[3] = ARMING_FLAG(OK_TO_ARM);

        warningLedUpdate();
    }

    // Read out gyro temperature. can use it for something somewhere. maybe get MCU temperature instead? lots of fun possibilities.
    if (gyro.temperature)
        gyro.temperature(&telemTemperature1);
}