本文整理了Java中us.ihmc.robotics.math.frames.YoFrameVector.getX()方法的一些代码示例，展示了YoFrameVector.getX()的具体用法。这些代码示例主要来源于Github/Stackoverflow/Maven等平台，是从一些精选项目中提取出来的代码，具有较强的参考意义，能在一定程度帮忙到你。YoFrameVector.getX()方法的具体详情如下：
包路径：us.ihmc.robotics.math.frames.YoFrameVector
类名称：YoFrameVector
方法名：getX

YoFrameVector.getX介绍

暂无

代码示例

代码示例来源：origin: us.ihmc/IHMCRoboticsToolkit

public double getAngularPartX()
{
 return angularPart.getX();
}

代码示例来源：origin: us.ihmc/IHMCRoboticsToolkit

public double getLinearPartX()
{
 return linearPart.getX();
}

代码示例来源：origin: us.ihmc/IHMCRoboticsToolkit

private void initializePolynomials()
{
 xPolynomial.setInitialPositionVelocityZeroFinalHighOrderDerivatives(0.0, trajectoryTime.getDoubleValue(), initialPosition.getX(), initialVelocity.getX(), finalPosition.getX(), finalVelocity.getX());
 yPolynomial.setInitialPositionVelocityZeroFinalHighOrderDerivatives(0.0, trajectoryTime.getDoubleValue(), initialPosition.getY(), initialVelocity.getY(), finalPosition.getY(), finalVelocity.getY());
 zPolynomial.setInitialPositionVelocityZeroFinalHighOrderDerivatives(0.0, trajectoryTime.getDoubleValue(), initialPosition.getZ(), initialVelocity.getZ(), finalPosition.getZ(), finalVelocity.getZ());
}

代码示例来源：origin: us.ihmc/DarpaRoboticsChallenge

groundContactPointsSlipper.setDoSlip(true);
translationPhase.setX(translationPhase.getX() + 2.0  * Math.PI * translationFreqHz[0] * deltaT);
translationPhase.setY(translationPhase.getY() + 2.0  * Math.PI * translationFreqHz[1] * deltaT);
translationPhase.setZ(translationPhase.getZ() + 2.0  * Math.PI * translationFreqHz[2] * deltaT);
rotationPhaseEuler.setX(rotationPhaseEuler.getX() + 2.0  * Math.PI * rotationFreqHzYawPitchRoll[2] * deltaT);
rotationPhaseEuler.setY(rotationPhaseEuler.getY() + 2.0  * Math.PI * rotationFreqHzYawPitchRoll[1] * deltaT);
rotationPhaseEuler.setZ(rotationPhaseEuler.getZ() + 2.0  * Math.PI * rotationFreqHzYawPitchRoll[0] * deltaT);
nextTranslationToSlip.setX(nextTranslationToSlip.getX() * (2.0 * Math.PI * translationFreqHz[0] * Math.sin(translationPhase.getX()) * deltaT));
nextTranslationToSlip.setY(nextTranslationToSlip.getY() * (2.0 * Math.PI * translationFreqHz[1] * Math.sin(translationPhase.getY()) * deltaT));
nextTranslationToSlip.setZ(nextTranslationToSlip.getZ() * (2.0 * Math.PI * translationFreqHz[2] * Math.sin(translationPhase.getZ()) * deltaT));
nextRotationToSlipEulerAngles.setX(nextRotationToSlipEulerAngles.getX() * (2.0 * Math.PI * rotationFreqHzYawPitchRoll[2] * Math.sin(rotationPhaseEuler.getX()) * deltaT));
nextRotationToSlipEulerAngles.setY(nextRotationToSlipEulerAngles.getY() * (2.0 * Math.PI * rotationFreqHzYawPitchRoll[1] * Math.sin(rotationPhaseEuler.getY()) * deltaT));
nextRotationToSlipEulerAngles.setZ(nextRotationToSlipEulerAngles.getZ() * (2.0 * Math.PI * rotationFreqHzYawPitchRoll[0] * Math.sin(rotationPhaseEuler.getZ()) * deltaT));

代码示例来源：origin: us.ihmc/IHMCSimulationToolkit

groundContactPointsSlipper.setDoSlip(true);
translationPhase.setX(translationPhase.getX() + 2.0  * Math.PI * translationFreqHz[0] * deltaT);
translationPhase.setY(translationPhase.getY() + 2.0  * Math.PI * translationFreqHz[1] * deltaT);
translationPhase.setZ(translationPhase.getZ() + 2.0  * Math.PI * translationFreqHz[2] * deltaT);
rotationPhaseEuler.setX(rotationPhaseEuler.getX() + 2.0  * Math.PI * rotationFreqHzYawPitchRoll[2] * deltaT);
rotationPhaseEuler.setY(rotationPhaseEuler.getY() + 2.0  * Math.PI * rotationFreqHzYawPitchRoll[1] * deltaT);
rotationPhaseEuler.setZ(rotationPhaseEuler.getZ() + 2.0  * Math.PI * rotationFreqHzYawPitchRoll[0] * deltaT);
nextTranslationToSlip.setX(nextTranslationToSlip.getX() * (2.0 * Math.PI * translationFreqHz[0] * Math.sin(translationPhase.getX()) * deltaT));
nextTranslationToSlip.setY(nextTranslationToSlip.getY() * (2.0 * Math.PI * translationFreqHz[1] * Math.sin(translationPhase.getY()) * deltaT));
nextTranslationToSlip.setZ(nextTranslationToSlip.getZ() * (2.0 * Math.PI * translationFreqHz[2] * Math.sin(translationPhase.getZ()) * deltaT));
nextRotationToSlipEulerAngles.setX(nextRotationToSlipEulerAngles.getX() * (2.0 * Math.PI * rotationFreqHzYawPitchRoll[2] * Math.sin(rotationPhaseEuler.getX()) * deltaT));
nextRotationToSlipEulerAngles.setY(nextRotationToSlipEulerAngles.getY() * (2.0 * Math.PI * rotationFreqHzYawPitchRoll[1] * Math.sin(rotationPhaseEuler.getY()) * deltaT));
nextRotationToSlipEulerAngles.setZ(nextRotationToSlipEulerAngles.getZ() * (2.0 * Math.PI * rotationFreqHzYawPitchRoll[0] * Math.sin(rotationPhaseEuler.getZ()) * deltaT));

代码示例来源：origin: us.ihmc/IHMCGraphicsDescription

public void set(YoFramePoint base, YoFrameVector vector)
{
 this.baseX.set(base.getX());
 this.baseY.set(base.getY());
 this.baseZ.set(base.getZ());
 this.x.set(vector.getX());
 this.y.set(vector.getY());
 this.z.set(vector.getZ());
}

代码示例来源：origin: us.ihmc/CommonWalkingControlModules

momentumRateCommand.setWeights(angularMomentumRateWeight.getX(), angularMomentumRateWeight.getY(), angularMomentumRateWeight.getZ(),
   linearMomentumRateWeight.getX(), linearMomentumRateWeight.getY(), linearMomentumRateWeight.getZ());

代码示例来源：origin: us.ihmc/IHMCRoboticsToolkit

private void computeIntegralTerm()
{
 if (gains.getMaximumIntegralError() < 1e-5)
 {
   integralTerm.setToZero(bodyFrame);
   return;
 }
 double errorIntegratedX = positionError.getX() * dt;
 double errorIntegratedY = positionError.getY() * dt;
 double errorIntegratedZ = positionError.getZ() * dt;
 positionErrorCumulated.add(errorIntegratedX, errorIntegratedY, errorIntegratedZ);
 double errorMagnitude = positionErrorCumulated.length();
 if (errorMagnitude > gains.getMaximumIntegralError())
 {
   positionErrorCumulated.scale(gains.getMaximumIntegralError() / errorMagnitude);
 }
 positionErrorCumulated.getFrameTuple(integralTerm);
 integralGainMatrix.transform(integralTerm.getVector());
}

代码示例来源：origin: us.ihmc/CommonWalkingControlModules

private void computeIntegralTerm(ReferenceFrame baseFrame)
{
 if (gains.getMaximumIntegralError() < 1e-5)
 {
   integralTerm.setToZero(baseFrame);
   return;
 }
 double errorIntegratedX = positionError.getX() * dt;
 double errorIntegratedY = positionError.getY() * dt;
 double errorIntegratedZ = positionError.getZ() * dt;
 positionErrorCumulated.add(errorIntegratedX, errorIntegratedY, errorIntegratedZ);
 double errorMagnitude = positionErrorCumulated.length();
 if (errorMagnitude > gains.getMaximumIntegralError())
 {
   positionErrorCumulated.scale(gains.getMaximumIntegralError() / errorMagnitude);
 }
 positionErrorCumulated.getFrameTupleIncludingFrame(integralTerm);
 integralTerm.changeFrame(baseFrame);
 integralGainMatrix.transform(integralTerm.getVector());
}

代码示例来源：origin: us.ihmc/IHMCRoboticsToolkit

@Override
public void initialize()
{
 currentTime.set(0.0);
 double tIntermediate = trajectoryTime.getDoubleValue() / 2.0;
 xPolynomial.setQuadraticWithFinalVelocityConstraint(0.0,trajectoryTime.getDoubleValue(), initialPosition.getX(), finalPosition.getX(), finalVelocity.getX());
 yPolynomial.setQuadraticWithFinalVelocityConstraint(0.0,trajectoryTime.getDoubleValue(), initialPosition.getY(), finalPosition.getY(), finalVelocity.getY());
 zPolynomial.setCubicWithIntermediatePositionAndFinalVelocityConstraint(0.0,  tIntermediate, trajectoryTime.getDoubleValue(), initialPosition.getZ(), intermediateZPosition.getDoubleValue(), finalPosition.getZ(), finalVelocity.getZ());
 currentPosition.set(initialPosition);
 currentAcceleration.setToZero();
}

代码示例来源：origin: us.ihmc/CommonWalkingControlModules

linearMomentumRateWeight.set(defaultLinearMomentumRateWeight);
momentumRateCommand.setWeights(0.0, 0.0, 0.0, linearMomentumRateWeight.getX(), linearMomentumRateWeight.getY(), linearMomentumRateWeight.getZ());

代码示例来源：origin: us.ihmc/CommonWalkingControlModules

measuredTorqueAtControlFrame.set(measuredTorque.getVector());
errorForce.setIncludingFrame(controlFrame, desiredForce.getX(), desiredForce.getY(), desiredForce.getZ());
errorForce.sub(measuredForce);
errorTorque.setIncludingFrame(controlFrame, desiredTorque.getX(), desiredTorque.getY(), desiredTorque.getZ());
errorTorque.sub(measuredTorque);