Kalman Filter: An Introduction

Kalman Filter is an algorithm used for the estimation of a system's state based on a series of measurements. It was developed by Rudolf Kalman in the 1960s and is widely used in a variety of fields, including engineering, economics, and biology. The Kalman Filter is designed to be a recursive algorithm that continuously updates the estimated state of the system as new measurements become available.

The Kalman Filter Algorithm

The Kalman Filter algorithm is based on a mathematical model of the system being estimated. This model consists of two parts: the state transition model and the measurement model. The state transition model describes how the system's state evolves over time, while the measurement model describes how measurements of the system are related to the state.

The Kalman Filter algorithm consists of two main steps: the prediction step and the update step. In the prediction step, the algorithm uses the state transition model to predict the state of the system at the next time step. In the update step, the algorithm uses the measurement model to update the predicted state based on the most recent measurement.

The prediction step can be summarized as follows:

  • Project the current state estimate ahead in time using the state transition model:

    x^k+1k=Fkx^kk+Bkuk\hat{x}_{k+1|k} = F_k \hat{x}_{k|k} + B_k u_k

    where x^kk\hat{x}_{k|k} is the current state estimate, FkF_k is the state transition matrix, BkB_k is the input matrix, and uku_k is the input vector.

  • Project the error covariance ahead in time:

    Pk+1k=FkPkkFkT+QkP_{k+1|k} = F_k P_{k|k} F_k^T + Q_k

    where PkkP_{k|k} is the current error covariance estimate, QkQ_k is the process noise covariance matrix.

The update step can be summarized as follows:

  • Compute the Kalman gain:

    Kk=PkkHkT(HkPkkHkT+Rk)1K_k = P_{k|k} H_k^T (H_k P_{k|k} H_k^T + R_k)^{-1}

    where HkH_k is the measurement matrix, RkR_k is the measurement noise covariance matrix.

  • Update the state estimate:

    x^kk+1=x^kk+Kk(ykHkx^kk)\hat{x}_{k|k+1} = \hat{x}_{k|k} + K_k (y_k - H_k \hat{x}_{k|k})

    where yky_k is the measurement at time step kk.

  • Update the error covariance estimate:

    Pkk+1=(IKkHk)PkkP_{k|k+1} = (I - K_k H_k) P_{k|k}

The Kalman Filter algorithm is designed to handle noisy measurements and uncertainties in the system model. The Kalman gain is used to balance the information from the measurement and the model prediction. The gain is weighted towards the measurement when its noise is small and the model prediction is unreliable, and is weighted towards the model prediction when the measurement noise is large and the model prediction is reliable.

Applications of Kalman Filter

Kalman Filter has a wide range of applications in many different fields. Some of the most common applications include:

  • Navigation and Localization: The Kalman Filter can be used to estimate the position, velocity, and orientation of a vehicle based on sensor measurements such as GPS and inertial sensors.

  • Control Systems: The Kalman Filter can be used to estimate the state of a control system and adjust the control variables to achieve a desired performance.

  • Signal Processing: The Kalman Filter can be used to filter out noise from signals and extract useful information.

  • Robotics: The Kalman Filter can be used to estimate the state of a robot based on sensor measurements and adjust its actions accordingly.

Conclusion

In conclusion, the Kalman Filter is a powerful algorithm that is widely used in many different fields. It is designed to estimate the state of a system based on a series of noisy measurements and uncertainties in the system model. The Kalman Filter algorithm is based on a mathematical model of the system being estimated and consists of two main steps: the prediction step and the update step. The Kalman Filter has many applications, including navigation and localization, control systems, signal processing, and robotics.

カルマンフィルター[JA]