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Kalman Filter Scalar Gain & Variance Update Calculator

The Kalman filter is the optimal recursive minimum mean-square error (MMSE) estimator for linear dynamical systems disturbed by Gaussian noise.

Predicted state from system dynamics model.

Uncertainty variance of the prior state prediction.

Observed noisy sensor measurement value.

Variance of sensor Gaussian measurement noise.

Calculated Result
0.6667

Optimal Kalman Gain (K)

Updated State Estimate (x̂)

11.3333

Updated Error Variance (P)

1.3333

Innovation Residual (y)

2.0000

Uncertainty Reduction

66.7%

Calculation Breakdown

  1. Innovation: y = z - x̂⁻12 - 10 = 2.0000
  2. Gain: K = P⁻ / (P⁻ + R)4 / (4 + 2) = 0.6667
  3. State: x̂ = x̂⁻ + K·y10 + 0.6667 × 2.0000 = 11.3333
  4. Variance: P = (1 - K)·P⁻(1 - 0.6667) × 4 = 1.3333

What Is the Kalman Filter Scalar Gain & Variance Update Calculator?

The Kalman filter provides real-time estimation of hidden state variables in the presence of noise.

The measurement update step optimally balances trust between model predictions and raw sensor data.

How Does the Kalman Filter Scalar Gain & Variance Update Calculator Work?

Calculates the innovation residual y = z - x_hat^-.

Determines the optimal Kalman gain K = P^- / (P^- + R).

Updates the state estimate x_hat and reduces error variance P.

Kalman Filter Scalar Gain & Variance Update Calculator Formula & Variables

The core mathematical equation utilized by this calculator is expressed as:

K = \frac{P^-}{P^- + R}, \quad \hat{x} = \hat{x}^- + K(z - \hat{x}^-), \quad P = (1 - K)P^-

Optimal Kalman measurement update equations for scalar linear observation.

How to Use the Kalman Filter Scalar Gain & Variance Update Calculator

  1. Enter prior predicted state and its associated uncertainty variance P^-.
  2. Enter the newly observed sensor measurement z.
  3. Provide the sensor noise variance R from sensor specifications.

Step-by-Step Example Calculation

GPS Velocity Tracking Fusion

Input Values:

priorEstimateXHatMinus:10
priorVariancePMinus:4
measurementZ:12
measurementNoiseVarianceR:2
Worked Steps: Fusing inertial dead-reckoning prediction with noisy GPS velocity fix.

Understanding Your Result

If sensor noise R is small, K approaches 1.0 and the filter trusts the measurement.

If model variance P^- is small, K approaches 0 and the filter rejects sensor noise.

Factors That Affect the Result

  • Sensor accuracy R: Lower sensor noise accelerates filter response to sudden state changes.
  • Process noise Q: Higher process uncertainty inflates prior variance P^-, increasing reliance on measurements.

When Should You Use This Calculator?

  • Avionics navigation, missile guidance, and autonomous vehicle trajectory tracking.
  • Sensor fusion combining IMU accelerometers, gyroscopes, and GPS receivers.

Assumptions & Limitations

  • Assumes linear observation model and zero-mean Gaussian white noise.
  • Applies to scalar (single-variable) state observations.

Frequently Asked Questions

Calculation Accuracy & Reference Note

Proven mathematically optimal minimum mean-square error estimator for linear Gaussian systems.

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