Title :
Image information based guidance system architecture for intercepting a maneuvring target
Author :
Fan, Y. ; Li, Q.D. ; Ren, Zhang ; Qi, P. ; Yang, Ping
Author_Institution :
Sci. & Technol. on Aircraft Control Lab., Beihang Univ., Beijing, China
Abstract :
A guidance system architecture for intercepting a manoeuvring target using a monocular imaging seeker is discussed in this paper. The relative interceptor-target kinematics based on the image information is established. A tracking differentiator (TD) based maneuvering target acceleration model is presented. The relative kinematic states can be obtained by combining this model with the extended Kalman filter, as the maneuvering mode of the target is unknown. In view of the maneuvring acceleration of the target can be treated as a time-varying and bounded perturbation, an adaptive guidance law is derived that guarantees the LOS rate to be global ultimate bounded in the presence of measurement noise during the terminal course. Simulation results show that the proposed guidance system architecture is effective and robust to the target maneuver.
Keywords :
Kalman filters; adaptive control; image processing; infrared imaging; missile guidance; nonlinear filters; perturbation techniques; target tracking; time-varying systems; LOS rate; adaptive guidance law; bounded perturbation; extended Kalman filter; image information based guidance system architecture; interceptor-target kinematics; monocular imaging seeker; time-varying perturbation; tracking differentiator based maneuvering target acceleration model; Acceleration; Adaptive systems; Imaging; Kalman filters; Kinematics; Navigation; Target tracking;
Conference_Titel :
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location :
Yantai
Print_ISBN :
978-1-4799-4700-3
DOI :
10.1109/CGNCC.2014.7007444