LSTM-based on-orbit identification of inertia tensor for space robot system

被引:0
|
作者
Chu W. [1 ]
Yang J. [1 ]
Wu S. [1 ]
Wu Z. [2 ]
机构
[1] School of Aeronautics and Astronautics, Dalian University of Technology, Dalian
[2] State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian
来源
Wu, Zhigang (wuzhg@dlut.edu.cn) | 1600年 / Chinese Society of Astronautics卷 / 42期
基金
中国国家自然科学基金;
关键词
Inertia tensor; Long-Short Term Memory (LSTM) network; On-orbit identification; Space robots; Target capture;
D O I
10.7527/S1000-6893.2020.24615
中图分类号
学科分类号
摘要
The system inertia tensor of the space robot is time-varying in the process of an out-of-control target capture and even undergoes abrupt changes at the moment of capture, seriously affecting the accuracy of its overall attitude control. To address the above problem, we propose an on-orbit real-time identification method for the system inertia tensor based on Long-Short Term Memory (LSTM). According to the two stages of pre-capture and post-capture, the dynamic model of the space robot is firstly developed using the Lagrangian equation. Based on the proposed model, the domain randomization method is then adopted to generate sufficient training data to train the parameter identification network constructed by an LSTM network and a multilayer fully connected network. Finally, the trained parameter identification network is used to identify the system inertia tensor. The test results demonstrate that the proposed method can accurately identify the system inertia tensor during the capture process of the space robot. The average relative identification error of the main moment of inertia is less than 0.001, and that of the product of inertia less than 0.01. © 2021, Beihang University Aerospace Knowledge Press. All right reserved.
引用
收藏
相关论文
共 21 条
  • [1] FLORES-ABAD A, MA O, PHAM K, Et al., A review of space robotics technologies for on-orbit servicing, Progress in Aerospace Sciences, 68, pp. 1-26, (2014)
  • [2] MENG Q L, LIANG J X, MA O., Identification of all the inertial parameters of a non-cooperative object in orbit, Aerospace Science and Technology, 91, pp. 571-582, (2019)
  • [3] BIONDI G, MAURO S, MOHTAR T, Et al., Attitude recovery from feature tracking for estimating angular rate of non-cooperative spacecraft, Mechanical Systems and Signal Processing, 83, pp. 321-336, (2017)
  • [4] MUROTSU Y, SENDA K, OZAKI M, Et al., Parameter identification of unknown object handled by free-flying space robot, Journal of Guidance, Control, and Dynamics, 17, 3, pp. 488-494, (1994)
  • [5] WANG M, HUANG P F, CHANG H T, Et al., On-orbit identification of inertia parameters of compound spacecraft using space manipulator, Journal of Northwestern Polytechnical University, 32, 5, pp. 811-816, (2014)
  • [6] HOU Z D, WANG Z K, ZHANG Y L., Research on identification of mass characteristics for spacecraft combination based on thrusters, Aerospace Control, 33, 1, pp. 54-60, (2015)
  • [7] ZHANG B, LIANG B, WANG X Q, Et al., Simulation of real-time dynamic parameter identification for large non-cooperative targets using adaptive reaction null space control, Robot, 38, 1, pp. 98-106, (2016)
  • [8] CHU Z Y, MA Y, HOU Y Y, Et al., Inertial parameter identification using contact force information for an unknown object captured by a space manipulator, Acta Astronautica, 131, pp. 69-82, (2017)
  • [9] XU W F, HU Z H, ZHANG Y, Et al., On-orbit identifying the inertia parameters of space robotic systems using simple equivalent dynamics, Acta Astronautica, 132, pp. 131-142, (2017)
  • [10] PUNJANI A, ABBEEL P., Deep learning helicopter dynamics models, 2015 IEEE International Conference on Robotics and Automation (ICRA), pp. 3223-3230, (2015)