This is an early access version, the complete PDF, HTML, and XML versions will be available soon.
Open AccessArticle
Coordinated Collision-Free Trajectory Planning for a Discrete-Serpentine Heterogeneous Dual-Arm Space Robot Based on Equivalent Kinematics
1
School of Mechanical & Automotive Engineering, Liaocheng University, Liaocheng 252000, China
2
School of Mechanical Engineering and Automation, Harbin Institute of Technology, Shenzhen 518055, China
3
School of Aeronautics and Astronautics, Shenzhen Campus, Sun Yat-sen University, Shenzhen 518107, China
*
Authors to whom correspondence should be addressed.
Aerospace 2026, 13(1), 34; https://doi.org/10.3390/aerospace13010034 (registering DOI)
Submission received: 5 November 2025
/
Revised: 6 December 2025
/
Accepted: 26 December 2025
/
Published: 28 December 2025
Abstract
Compared with a single discrete or serpentine arm, the discrete-serpentine heterogeneous dual-arm space robot (DSHDASR) combines the advantages of both kinds of arms, enabling it to perform complex on-orbit missions. The structural complexity of DSHDASR and cluttered environments pose a significant challenge in modeling and collision-free motion planning. To tackle the issue, this paper proposes a coordinated collision-free trajectory planning method for DSHDASR based on equivalent kinematics. Firstly, the mechanism and universal kinematics of DSHDASR are analyzed. Then, the equivalent kinematics model is established based on the spatial arc method. The whole kinematics chain of DSHDASR is described by the parameters of equivalent curves composed of space arcs. Furthermore, taking the target satellite transposition as an example, a coordinated collision-free trajectory planning is presented for DSHDASR based on the equivalent kinematics. The trajectory planning problem is formulated as the minimization of the objective function, which consists of kinematics constraint equations and obstacle avoidance constraint equations. The parameters of equivalent curves are obtained by optimizing the objective function, and the joint angles of DSHDASR can be determined using the above parameters. Finally, the mission of the target satellite transposition is simulated, and the results demonstrate the proposed method.
Share and Cite
MDPI and ACS Style
Hu, Z.; Pu, Z.; Xu, W.; Li, W.; Meng, D.
Coordinated Collision-Free Trajectory Planning for a Discrete-Serpentine Heterogeneous Dual-Arm Space Robot Based on Equivalent Kinematics. Aerospace 2026, 13, 34.
https://doi.org/10.3390/aerospace13010034
AMA Style
Hu Z, Pu Z, Xu W, Li W, Meng D.
Coordinated Collision-Free Trajectory Planning for a Discrete-Serpentine Heterogeneous Dual-Arm Space Robot Based on Equivalent Kinematics. Aerospace. 2026; 13(1):34.
https://doi.org/10.3390/aerospace13010034
Chicago/Turabian Style
Hu, Zhonghua, Zhonghan Pu, Wenfu Xu, Wenshuo Li, and Deshan Meng.
2026. "Coordinated Collision-Free Trajectory Planning for a Discrete-Serpentine Heterogeneous Dual-Arm Space Robot Based on Equivalent Kinematics" Aerospace 13, no. 1: 34.
https://doi.org/10.3390/aerospace13010034
APA Style
Hu, Z., Pu, Z., Xu, W., Li, W., & Meng, D.
(2026). Coordinated Collision-Free Trajectory Planning for a Discrete-Serpentine Heterogeneous Dual-Arm Space Robot Based on Equivalent Kinematics. Aerospace, 13(1), 34.
https://doi.org/10.3390/aerospace13010034
Note that from the first issue of 2016, this journal uses article numbers instead of page numbers. See further details
here.
Article Metrics
Article metric data becomes available approximately 24 hours after publication online.