Rendezvous and Docking Digital Simulation System Based on Matlab

Authors

An Hao, Space Control and Inertial Technology Research Center, Harbin Institute of Technology, Harbin 150001, China;
Zhenshen Qu, Space Control and Inertial Technology Research Center, Harbin Institute of Technology, Harbin 150001, China;
Changhong Wang, Space Control and Inertial Technology Research Center, Harbin Institute of Technology, Harbin 150001, China;

Abstract

Abstract: On the background of lunar orbit rendezvous and docking (RVD), a framework of the simulation system was designed. The dynamics, navigation and controller of the RVD system were built in detail, and a Simulink model of the lunar orbit RVD was established based on these results. A user interface and a 3D dynamic demonstration were designed to make the operation convenient and intuitive.The digital simulation system can be used to verify the lunar orbit RVD missions incipiently. Furthermore,a semi-physical RVD simulation was taken by using the modified model. The simulation results show the effectiveness of the inertia-visual integrated navigation and the good portability of the digital simulation system.

Recommended Citation

Hao, An; Qu, Zhenshen; and Wang, Changhong (2021) "Rendezvous and Docking Digital Simulation System Based on Matlab," Journal of System Simulation: Vol. 27: Iss. 6, Article 11.
DOI: 10.16182/j.cnki.joss.2015.06.011
Available at: https://dc-china-simulation.researchcommons.org/journal/vol27/iss6/11

First Page

1227

Revised Date

2014-09-19

DOI Link

https://doi.org/10.16182/j.cnki.joss.2015.06.011

Last Page

1234

CLC

V411.8

Recommended Citation

An Hao, Qu Zhenshen, Wang Changhong. Rendezvous and Docking Digital Simulation System Based on Matlab[J]. Journal of System Simulation, 2015, 27(6): 1227-1234.

DOI

10.16182/j.cnki.joss.2015.06.011