The Modeling and Simulation of Rendezvous and Docking

Author

Xia, Zhao ; Yu-Xian, Jiang ; Yun-Jie, Wu

Volume

3

fYear

2010

Firstpage

280

Lastpage

284

Abstract

The modeling and simulation of rendezvous and docking (R&D) are realized. The line of sight (LOS) dynamic model is built to describe the relative motion of R&D. The above model is used to research the changing of distance, pitch, and azimuth of LOS. The non-control system can´t accomplish R&D automatically. The sliding mode control is used to accomplish the flying around phase of R&D. Then, the control system is simulated. The results show the variables are all transferred to the final state successfully and the relative trajectory is desirable. Therefore, the model and control method are both effective for R&D.

Keywords

aerospace control; modelling; simulation; variable structure systems; LOS dynamic model; docking simulation; line of sight; noncontrol system; relative trajectory; rendezvous modeling; rendezvous simulation; sliding mode control; Aerodynamics; Azimuth; Computational modeling; Computer simulation; Control system synthesis; Educational institutions; Equations; Research and development; Sliding mode control; Space vehicles; LOS dynamic model; R&D; sliding mode control;

fLanguage

English

Publisher

ieee

Conference_Titel

Computer Modeling and Simulation, 2010. ICCMS '10. Second International Conference on

Conference_Location

Sanya, Hainan

Print_ISBN

978-1-4244-5642-0

Electronic_ISBN

978-1-4244-5643-7

Type

conf

DOI

10.1109/ICCMS.2010.430

Filename

5421227