DocumentCode
64666
Title
Kinematic Algorithms and Robust Controller Design for Inertially Stabilized System
Author
Seongil Hong ; Ki Dae Cho
Author_Institution
Agency for Defense Dev., Daejeon, South Korea
Volume
19
Issue
1
fYear
2014
fDate
Feb. 2014
Firstpage
76
Lastpage
87
Abstract
This paper describes a controller design method for the inertially stabilized system of a tracking radar. Its aim is to track a reference target trajectory with high accuracy while isolating rigid body rotational motions of a host ship. First, we investigate the trajectory generation problem to make the control input for a target tracking on the moving base. Second, dynamic equations of motion are formulated by the spring-mass-damper system to include rigid body dynamics as well as structural flexibility. The unknown parameters of dynamic equations are estimated with experimental input and output data by minimizing a predicted error. Third, mixed sensitivity H∞ robust controllers are designed to meet the conflict requirements of robustness and performance in the face of uncertainty. Finally, the proposed optimal controllers demonstrate the effectiveness of design methodology, and show high performance by numerical and experimental results.
Keywords
H∞ control; control system synthesis; kinematics; radar tracking; robust control; ships; shock absorbers; H∞ robust controllers; controller design method; dynamic equations; host ship; inertially stabilized system; kinematic algorithms; optimal controllers; rigid body dynamics; rigid body rotational motions; robust controller design; spring-mass-damper system; structural flexibility; tracking radar; trajectory generation problem; Azimuth; Kinematics; Marine vehicles; Radar tracking; Target tracking; Trajectory; Inertially stabilized system (ISS); inverse kinematics; mixed sensitivity robust control; parameter estimation; tracking radar;
fLanguage
English
Journal_Title
Mechatronics, IEEE/ASME Transactions on
Publisher
ieee
ISSN
1083-4435
Type
jour
DOI
10.1109/TMECH.2012.2223228
Filename
6341843
Link To Document