DocumentCode
2097359
Title
ADRC based integrated guidance and control scheme for the interception of maneuvering targets with desired LOS angle
Author
Zhao Chunzhe ; Huang Yi
Author_Institution
Key Lab. of Syst. & Control, Acad. of Math. & Syst. Sci., Beijing, China
fYear
2010
fDate
29-31 July 2010
Firstpage
6192
Lastpage
6196
Abstract
Based on the idea of the active disturbance rejection control (ADRC), an integrated guidance and control scheme is developed for the interception of maneuvering targets with the requested line-of-sight (LOS) angle. The ADRC based guidance law takes into account the nonlinearities and uncertainties involved both in the target kinematics and interceptor dynamics such that it can produce the acceleration which can realize the desired LOS angle even when the target is maneuvering. The ADRC based control law takes into account the nonlinearities and uncertainties existing in the motion dynamics such that the acceleration needed can be achieved. Furthermore, the capability of the proposed scheme is analyzed and the feasibility is tested by some simulations.
Keywords
aerospace control; control nonlinearities; kinematics; ADRC based control law; ADRC based integrated guidance; LOS angle; active disturbance rejection control; interceptor dynamics; line-of-sight angle; maneuvering target; motion dynamics; nonlinearity; target kinematics; Acceleration; Aerodynamics; Control systems; Missiles; Navigation; Uncertainty; Control Design for Nonlinear Uncertain Systems; Guidance Law for Maneuvering Targets; Integrated Guidance and Control; LOS Angle Constraints; the Active Disturbance Rejection Control (ADRC);
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2010 29th Chinese
Conference_Location
Beijing
Print_ISBN
978-1-4244-6263-6
Type
conf
Filename
5573050
Link To Document