An X, Y, Z Kalman tracking filter is described and its steady state characteristics are analytically determined when the radar sensor meaures range, bearing, and elevation (ϒ, θ, ϕ) at uniform intervals of time, T seconds. The relationship between the quantities measured by the sensor (ϒ,θ ,ϕ) and the Cartesian coordinate system (X, Y, Z) is explicitly considered.
Steady State Results for the X, Y, Z Kalman Tracking Filter
IEEE Transactions on Aerospace and Electronic Systems ; AES-13 , 4 ; 419-423
1977-07-01
549351 byte
Article (Journal)
Electronic Resource
English