Abstract

For trajectory planning problem with multiconstraints of free-floating space robots (FFSR), the optimal solution may be unavailable due to strict constraints. In order to avoid identify a solution and obtain an executable joint trajectory, this paper proposes a trajectory planning method based on dual-mode switching. Using this method, the planner can automatically switch between the optimal mode and the effective mode, and obtain a feasible joint trajectory that satisfies the task requirements when the end-effector tracking error constraint and the joint torque constraint are considered. In this paper, the multiconstraints model of FFSR, which mainly consider control and dynamic constraints and the trajectory planning model based on dual-mode switching, are established, and the corresponding solving method is presented. The simulation results demonstrate that the proposed method is effective and feasible.

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Data Availability Statement

Some or all data, models, or code that support the findings of this study are available from the corresponding author upon reasonable request.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 35Issue 3May 2022

History

Received: Jan 3, 2021
Accepted: Oct 29, 2021
Published online: Feb 25, 2022
Published in print: May 1, 2022
Discussion open until: Jul 25, 2022

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Professor, National Key Laboratory of Aerospace Flight Dynamics, School of Astronautics, Northwestern Polytechnical Univ., Xi’an 710072, China (corresponding author). ORCID: https://orcid.org/0000-0001-7934-1729. Email: [email protected]
Master’s Candidate, National Key Laboratory of Aerospace Flight Dynamics, School of Astronautics, Northwestern Polytechnical Univ., Xi’an 710072, China. Email: [email protected]
Guanghui Zhang [email protected]
Postgraduate Researcher, First Research Laboratory, AVIC Computing Technique Research Institute, Xi’an 710068, China. Email: [email protected]
Master’s Candidate, National Key Laboratory of Aerospace Flight Dynamics, School of Astronautics, Northwestern Polytechnical Univ., Xi’an 710072, China. Email: [email protected]
Mingming Wang [email protected]
Assistant Professor, National Key Laboratory of Aerospace Flight Dynamics, School of Astronautics, Northwestern Polytechnical Univ., Xi’an 710072, China. Email: [email protected]
Jianping Yuan [email protected]
Professor, National Key Laboratory of Aerospace Flight Dynamics, School of Astronautics, Northwestern Polytechnical Univ., Xi’an 710072, China. Email: [email protected]

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