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 :
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