AEROSPACE SHANGHAI, Volume. 42, Issue 3, 137(2025)
Input Shaping Control Method for Transporting Assembly Modules of Space Robots
[1] D LI, L ZHONG, W ZHU et al. A Survey of space robotic technologies for on-orbit assembly. Space:Science & Technology, 325-337(2022).
[5] Z XUE, J LIU, C WU et al. Review of in-space assembly technologies. Chinese Journal of Aeronautics, 34, 21-47(2021).
[10] B WANG, Z LIU, P ZHENG. Rigid-flexible coupling dynamic modeling and analysis of dumbbell-shaped spacecraft. Aerospace Science and Technology, 126, 107641(2022).
[12] J DE. Twenty-five years of natural coordinates. Multibody System Dynamics, 18, 15-33(2007).
[13] X SUN, M XU, R ZHONG. Dynamic analysis of the tether transportation system using absolute nodal coordinate formulation. Acta Astronautica, 139, 266-277(2017).
[16] G JIANG, J JIANG, G YANG et al. Orbit-attitude-structure coupled modelling method in local translational coordinate frame for multibody systems. International Journal of Non-Linear Mechanics, 157, 104562(2023).
[17] H WEN, T CHEN, B YU et al. Dynamics and control of robotic spacecrafts for the transportation of flexible elements. Journal of Physics.Conference Series, 744, 12060(2016).
[18] Y KAWAI, T ENDO, F MATSUNO. Cooperative control of large flexible space structure by two planar robots. IET Control Theory & Applications, 15, 771-783(2021).
[19] P BONING, S DUBOWSKY. Coordinated control of space robot teams for the on-orbit construction of large flexible space structures. Advanced Robotics, 24, 303-323(2010).
[20] Y ISHIJIMA, D TZERANIS, S DUBOWSKY. The on-orbit maneuvering of large space flexible structures by free-flying robots, 1-6(2005).
[22] M YAO, X XIAO, Y TIAN et al. A two-time scale control scheme for on-orbit manipulation of large flexible module. Acta Astronautica, 154, 92-102(2019).
[23] Z QIU, G CHEN, X ZHANG. Trajectory planning and vibration control of translation flexible hinged plate based on optimization and reinforcement learning algorithm. Mechanical Systems and Signal Processing, 179, 109362(2022).
[24] H D THO, A KANESHIGE, K TERASHIMA. Minimum-time S-curve commands for vibration-free transportation of an overhead crane with actuator limits. Control Engineering Practice, 98, 104390(2020).
[25] Y LIU, X LIU, G CAI et al. Trajectory planning and coordination control of a space robot for detumbling a flexible tumbling target in post-capture phase. Multibody System Dynamics, 52, 281-311(2021).
[26] S PARMAN, T H GO. Two constant amplitude pulses’ input shaper to maneuver an attitude of precise-oriented flexible spacecraft. Journal of Sound and Vibration, 465, 115011(2020).
[28] T CHEN, Y WANG, H WEN et al. Autonomous assembly of multiple flexible spacecraft using RRT algorithm and input shaping technique. Nonlinear Dynamics, 111, 11223-11241(2023).
[29] P GASBARRI, R MONTI, M SABATINI. Very large space structures:non-linear control and robustness to structural uncertainties. Acta Astronautica, 93, 252-265(2014).
[30] J WANG, D LI. Optimal Variable Amplitudes Input Shaping Control for Slew Maneuver of Flexible Spacecraft, 105-137(2021).
[31] J ZHAO, Q TIAN, H HU. Modal analysis of a rotating thin plate via absolute nodal coordinate formulation. Journal of Computational and Nonlinear Dynamics, 6(2011).
[32] A M MIKKOLA, A A SHABANA. A non-incremental finite element procedure for the analysis of large deformation of plates and shells in mechanical system applications. Multibody System Dynamics, 9, 283-309(2003).
[33] Q LI, Z DENG, K ZHANG et al. Unified modeling method for large space structures using absolute nodal coordinate. AIAA Journal, 56, 4140-4157(2018).
[34] J SHAN, H LIU, D SUN. Modified input shaping for a rotating single-link flexible manipulator. Journal of Sound and Vibration, 285, 187-207(2005).
Get Citation
Copy Citation Text
Xu CHENG, Jianping JIANG, Guoqi JIANG, Qingjun LI, Zhiyuan WANG, Zhiqin ZHUO. Input Shaping Control Method for Transporting Assembly Modules of Space Robots[J]. AEROSPACE SHANGHAI, 2025, 42(3): 137
Category: Guidance, Navigation, Control and Electronics
Received: Sep. 23, 2024
Accepted: --
Published Online: Sep. 29, 2025
The Author Email: