DocumentCode :
1735606
Title :
3D target tracking by UAVs subject to measurement uncertainties
Author :
Subbarao, Kamesh ; Ahmed, Mousumi
Author_Institution :
Dept. of Mech. & Aerosp. Eng., Univ. of Texas at Arlington, Arlington, TX, USA
fYear :
2011
Firstpage :
687
Lastpage :
692
Abstract :
This paper proposes an Extended Kalman Filter (EKF) based approach to track a moving target UAV in 3D. The state of the target UAV is estimated from the range, azimuth, and elevation angle measurements that are assumed to be available from a ground based sensor or from on-board seeker antenna. The chaser vehicle states are also estimated using onboard sensors, namely GPS + IMU. These estimated states (chaser and the target) are utilized in a nonlinear guidance law which provides signals for the velocity, flight path, and course/heading angle to the chaser so as to track the target vehicle. It is to be mentioned that the guidance controller onboard the chaser was designed based on a backstepping like technique. All process and measurement noise are modelled as zero-mean Gaussian processes with known covariances. The performance of the combined estimation and guidance algorithm is shown via extensive simulation.
Keywords :
Gaussian processes; Global Positioning System; Kalman filters; aerospace control; mobile robots; remotely operated vehicles; sensors; target tracking; 3D target tracking; EKF; UAV subject; backstepping like technique; elevation angle measurements; extended Kalman Filter; ground based sensor; guidance controller; measurement uncertainties; noise measurement; nonlinear guidance law; onboard seeker antenna; zero-mean Gaussian processes; Estimation; Kalman filters; Mathematical model; Noise; Noise measurement; Target tracking; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Applications (CCA), 2011 IEEE International Conference on
Conference_Location :
Denver, CO
Print_ISBN :
978-1-4577-1062-9
Electronic_ISBN :
978-1-4577-1061-2
Type :
conf
DOI :
10.1109/CCA.2011.6044399
Filename :
6044399
Link To Document :
بازگشت