Optimum Steady State Position, Velocity, and Acceleration Estimation Using Noisy Sampled Position Data
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A one-dimensional tracking filter based on the Kalman filtering techniques for tracking of a dynamic target such as an aircraft is discussed. The target is assumed to be moving with constant acceleration and is acted upon by a plant noise which perturbs its constant acceleration motion. The plant noise accounts for maneuvers and/or other random factors. Analytical results for estimating optimum steady state position, velocity, and acceleration of the target are obtained.
[1] F.R Castella,et al. Analytical Results for the x, y Kalman Tracking Filter , 1974, IEEE Transactions on Aerospace and Electronic Systems.
[2] K. Ramachandra,et al. Steady State Results for the X, Y, Z Kalman Tracking Filter , 1977, IEEE Transactions on Aerospace and Electronic Systems.
[3] B. Friedland. Optimum Steady-State Position and Velocity Estimation Using Noisy Sampled Position Data , 1973, IEEE Transactions on Aerospace and Electronic Systems.