diff options
| -rw-r--r-- | src/modules/fw_pos_control_l1/mtecs/mTecs.cpp | 6 |
1 files changed, 3 insertions, 3 deletions
diff --git a/src/modules/fw_pos_control_l1/mtecs/mTecs.cpp b/src/modules/fw_pos_control_l1/mtecs/mTecs.cpp index 94a614bc0..087e1b476 100644 --- a/src/modules/fw_pos_control_l1/mtecs/mTecs.cpp +++ b/src/modules/fw_pos_control_l1/mtecs/mTecs.cpp @@ -160,15 +160,15 @@ int mTecs::updateFlightPathAngleAcceleration(float flightPathAngle, float flight float airspeedDerivativeNorm = airspeedDerivative / CONSTANTS_ONE_G; float airspeedDerivativeSp = accelerationLongitudinalSp; float airspeedDerivativeNormSp = airspeedDerivativeSp / CONSTANTS_ONE_G; - float airspeedDerivativeNormErrorSp = airspeedDerivativeNormSp - airspeedDerivativeNorm; + float airspeedDerivativeNormError = airspeedDerivativeNormSp - airspeedDerivativeNorm; float totalEnergyRate = flightPathAngle + airspeedDerivativeNorm; - float totalEnergyRateError = flightPathAngleError + airspeedDerivativeNormErrorSp; + float totalEnergyRateError = flightPathAngleError + airspeedDerivativeNormError; float totalEnergyRateSp = flightPathAngleSp + airspeedDerivativeNormSp; float totalEnergyRateError2 = totalEnergyRateSp - totalEnergyRate; float energyDistributionRate = flightPathAngle - airspeedDerivativeNorm; - float energyDistributionRateError = flightPathAngleError - airspeedDerivativeNormErrorSp; + float energyDistributionRateError = flightPathAngleError - airspeedDerivativeNormError; float energyDistributionRateSp = flightPathAngleSp - airspeedDerivativeNormSp; float energyDistributionRateError2 = energyDistributionRateSp - energyDistributionRate; |