DocumentCode :
299986
Title :
Adaptive control of space robot system with an attitude controlled base
Author :
Ma, Baoli ; Huo, Wei
Author_Institution :
Seventh Res. Div., Beijing Univ. of Aeronaut. & Astronaut., China
Volume :
2
fYear :
1995
fDate :
21-27 May 1995
Firstpage :
1265
Abstract :
The paper investigates the adaptive control of the space robot system with an attitude controlled base on which the robot is attached. We discuss the issues associated with adaptive control in inertial space and identify two potential problems: unavailability of joint trajectory, and nonlinear parameterization of system dynamics in inertial space. Two adaptive control schemes, corresponding to availability and unavailability of joint acceleration measurement, are proposed inspired by the fact that the dynamics in joint space and the kinematics can both be linearly parameterized. The proposed adaptive schemes guarantee the zero end-effector position tracking error, and the zero end-effector velocity tracking error is also guaranteed when the joint acceleration measurement is available. The validity and effectiveness of the proposed control schemes are demonstrated by the simulation of two-link planar space manipulator system
Keywords :
acceleration; adaptive control; attitude control; manipulator dynamics; manipulator kinematics; tracking; adaptive control; attitude control; inertial space; joint acceleration; joint trajectory; kinematics; nonlinear parameterization; position tracking error; space robot system; system dynamics; two-link planar space manipulator; velocity tracking error; Accelerometers; Adaptive control; Aerodynamics; Attitude control; Control systems; Nonlinear dynamical systems; Orbital robotics; Robot kinematics; Space stations; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Robotics and Automation, 1995. Proceedings., 1995 IEEE International Conference on
Conference_Location :
Nagoya
ISSN :
1050-4729
Print_ISBN :
0-7803-1965-6
Type :
conf
DOI :
10.1109/ROBOT.1995.525455
Filename :
525455
Link To Document :
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