원문정보
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초록
영어
This paper introduces the components and functions of institution aiming at docking capture link of the small satellite manipulator end executor. Putting forward to Euler method and quaternion as the theoretical basis, kinetics of grasping institution the relative position and attitude are modeling and analyzed. The axial tilt grab conditions of the simulation analysis are finished by the ADAMS software. The results of the simulation analysis for the relative position and velocity and the hand-grasp collision force are concluded.
목차
Abstract
1. Introduction
2. The Components and Functions of Grasping Institution
3. The Relative Position and Attitude Determine of the Grasping Mechanism and Establishment of the Kinematics Model
3.1. Definition the Coordinate System of the Grasping Mechanism
3.2. The Introduction and Transformation Attitude Parameters
4. Dynamic Modeling and Analysis of Grasping Mechanism the Relative Position and Attitude
4.1. Dynamic Modeling and Analysis of Grasping Mechanism the Relative Position
4.2. Dynamic Modeling and Analysis of Grasping Mechanism Attitude
5. The Simulation Results of the End Executor Grasping Mechanism during the Grasping Process
6. Conclusion
Acknowledgments
References
1. Introduction
2. The Components and Functions of Grasping Institution
3. The Relative Position and Attitude Determine of the Grasping Mechanism and Establishment of the Kinematics Model
3.1. Definition the Coordinate System of the Grasping Mechanism
3.2. The Introduction and Transformation Attitude Parameters
4. Dynamic Modeling and Analysis of Grasping Mechanism the Relative Position and Attitude
4.1. Dynamic Modeling and Analysis of Grasping Mechanism the Relative Position
4.2. Dynamic Modeling and Analysis of Grasping Mechanism Attitude
5. The Simulation Results of the End Executor Grasping Mechanism during the Grasping Process
6. Conclusion
Acknowledgments
References
저자정보
참고문헌
자료제공 : 네이버학술정보