Title :
Optimization of observer trajectories for bearings-only target localization
Author :
Oshman, Yaakov ; Davidson, Pavel
Author_Institution :
Dept. of Aerosp. Eng., Technion-Israel Inst. of Technol., Haifa, Israel
fDate :
7/1/1999 12:00:00 AM
Abstract :
The problem of bearings-only target localization is to estimate the location of a fixed target from a sequence of noisy bearing measurements. Although, in theory, this process is observable even without an observer maneuver, estimation performance (i.e., accuracy, stability and convergence rate) can be greatly enhanced by properly exploiting observer motion to increase observability. This work addresses the optimization of observer trajectories for bearings-only fixed-target localization. The approach presented herein is based on maximizing the determinant of the Fisher information matrix (FIM), subject to state constraints imposed on the observer trajectory (e.g., by the target defense system). Direct optimal control numerical schemes, including the recently introduced differential inclusion (DI) method, are used to solve the resulting optimal control problem. Computer simulations, utilizing the familiar Stansfield and maximum likelihood (ML) estimators, demonstrate the enhancement to target position estimability using the optimal observer trajectories
Keywords :
adaptive estimation; direction-of-arrival estimation; gradient methods; maximum likelihood estimation; observability; observers; optimal control; optimisation; target tracking; Fisher information matrix; Stansfield estimator; bearings-only target localization; convergence rate; differential inclusion method; direct gradient based method; direct optimal control numerical schemes; fixed target location; hard state constraints; maximum likelihood estimator; noisy bearing measurements; observability; observer motion; observer trajectories; optimal trajectories; optimization; state constraints; target position estimability; Computer simulation; Maximum likelihood estimation; Motion estimation; Observability; Observers; Optimal control; Performance analysis; Research and development; Stability; Trajectory;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on