Analysis and control of a Stewart platform as base motion compensators - Part I: Kinematics using moving frames

• Published in: Nonlinear dynamics Vol. 107; no. 1; pp. 51 - 76
• Main Authors: Ono, Takeyuki, Eto, Ryosuke, Yamakawa, Junya, Murakami, Hidenori
• Format: Journal Article
• Language: English
• Published: Dordrecht Springer Netherlands 2022; Springer Nature B.V
• Subjects: Automotive Engineering; Center of mass; Classical Mechanics; Closed loops; Compensators; Control; Dynamical Systems; Engineering; Frames; Graph theory; Inertial coordinates; Inverse dynamics; Inverse kinematics; Kinematics; Lie groups; Mathematical analysis; Mechanical Engineering; Original Paper; Rotating bodies; Rotation; Scale models; Vibration; Base-moving Stewart platform; Inverse kinematics control; Moving frame method; Lie group; Motion compensation
• ISSN: 0924-090X; 1573-269X
• DOI: 10.1007/s11071-021-06767-8

Kinematics and its control application are presented for a Stewart platform whose base plate is installed on a floor in a moving ship or a vehicle. With a manipulator or a sensitive equipment mounted on the top plate, a Stewart platform is utilized to mitigate the undesirable motion of its base plate by controlling actuated translational joints on six legs. To reveal closed loops, a directed graph is utilized to express the joint connections. Then, kinematics begins by attaching an orthonormal coordinate system to each body at its center of mass and to each joint to define moving coordinate frames . Using the moving frames, each body in the configuration space is represented by an inertial position vector of its center of mass in the three-dimensional vector space ℝ 3 , and a rotation matrix of the body-attached coordinate axes. The set of differentiable rotation matrices forms a Lie group: the special orthogonal group , SO (3). The connections of body-attached moving frames are mathematically expressed by using frame connection matrices , which belong to another Lie group: the special Euclidean group , SE (3). The employment of SO (3) and SE (3) facilitates effective matrix computations of velocities of body-attached coordinate frames. Loop closure constrains are expressed in matrix form and solved analytically for inverse kinematics . Finally, experimental results of an inverse kinematics control are presented for a scale model of a base-moving Stewart platform. Dynamics and a control application of inverse dynamics are presented in the part II-paper.