Title :
Optimum Steady State Position, Velocity, and Acceleration Estimation Using Noisy Sampled Position Data
Author :
Ramachandra, K.V.
Author_Institution :
Electronics and Radar Development Estblishment DRDO Complex, Byrasandra Bangalore 560075 India
Abstract :
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.
Keywords :
Acceleration; Aircraft; Equations; Gain measurement; Kalman filters; Noise measurement; Position measurement; Q measurement; State estimation; Steady-state;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
DOI :
10.1109/TAES.1987.310865