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Dual Quaternion Framework for Modeling of Spacecraft-Mounted Multibody Robotic Systems.
Alfredo Valverde1, Panagiotis Tsiotras1
1Dynamics and Control Systems Laboratory, School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, GA, United States.
This study presents a dual quaternion framework for modeling spacecraft robotic systems. It unifies rotational and translational dynamics for improved kinematic and dynamic analysis.
Area of Science:
- Robotics
- Spacecraft Dynamics
- Multibody Systems
Background:
- Modeling complex robotic systems mounted on spacecraft presents challenges in unifying rotational and translational dynamics.
- Previous methods often require joint-type specific terms, complicating the analysis and decoupling motion components.
Purpose of the Study:
- To develop a unified framework for modeling the kinematics and dynamics of rigid spacecraft-mounted multibody robotic systems.
- To leverage dual quaternion algebra for a compact and integrated representation of motion.
Main Methods:
- The framework employs dual quaternion algebra for a unified representation of rotation and translation.
- A Newton-Euler formulation is used to establish a system of equations.
- The model incorporates five different joint types through adaptable mapping matrices.
Main Results:
- The proposed framework successfully models the kinematics and dynamics of multibody robotic systems on spacecraft.
- Dual quaternion algebra provides a compact representation, unifying rotational and translational aspects.
- The method simplifies the inclusion of various joint types without requiring joint-specific terms.
Conclusions:
- The dual quaternion-based framework offers a unified and efficient approach to modeling spacecraft robotic systems.
- This method overcomes limitations of previous approaches by integrating rotational and translational dynamics seamlessly.
- The framework's adaptability to different joint types enhances its applicability in space robotics research.
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