DocumentCode
2645945
Title
Object-oriented modelling for spacecraft dynamics: A case study
Author
Lovera, Marco ; Pulecchi, Tiziano
Author_Institution
Dipartimento di Elettronica e Informazione, Politecnico di Milano, Piazza Leonardo da Vinci 32, 20133, Italy
fYear
2006
fDate
4-6 Oct. 2006
Firstpage
1898
Lastpage
1903
Abstract
The development process for spacecraft control systems relies heavily on modelling and simulation tools for spacecraft dynamics. For this reason, there is an increasing need for adequate design tools in order to cope efficiently with tightening budgets for space missions. The aim of this paper is to discuss the main issues related to the modelling and simulation of satellite dynamics for control purposes, to present the results obtained so far in developing a Modelica library for spacecraft modelling and simulation and to illustrate them with a case study, currently being carried out for the SWARM ESA mission.
Keywords
Attitude control; Control system synthesis; Control systems; Libraries; Mathematical model; Object oriented modeling; Satellites; Space missions; Space vehicles; Vehicle dynamics;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer Aided Control System Design, 2006 IEEE International Conference on Control Applications, 2006 IEEE International Symposium on Intelligent Control, 2006 IEEE
Conference_Location
Munich, Germany
Print_ISBN
0-7803-9797-5
Electronic_ISBN
0-7803-9797-5
Type
conf
DOI
10.1109/CACSD-CCA-ISIC.2006.4776930
Filename
4776930
Link To Document