DocumentCode
619691
Title
Hybrid modeling and predictive control of a fractionated satellite system: A mixed logical dynamical approach
Author
Xiaoping Shi ; Hailong Liu ; Long Li
Author_Institution
Control & Simulation Center, Harbin Inst. of Technol., Harbin, China
fYear
2013
fDate
25-27 May 2013
Firstpage
198
Lastpage
203
Abstract
This paper proposes a model and predictive control of a fractionated satellite system by using Mixed Logic Dynamical (MLD) approach. The power management system of a fractionated satellite can be seen as a hybrid system, which includes discrete dynamics, continuous dynamics, and logic rules. Discrete features of the power management system are the different types of flight modes and discrete inputs. On the other hand, continuous dynamics feature is power consumption process in each mode. The union of these properties characterizes the hybrid behavior of a power management system. In order to model both the discrete/continuous dynamics and the switching between different flight modes, the MLD framework has been exploiting. Then, predictive control scheme is proposed to control this hybrid system. To illustrate the effectiveness of the proposed approach, some numerical simulations are shown.
Keywords
aerospace control; artificial satellites; numerical analysis; power consumption; predictive control; MLD approach; continuous dynamics; discrete dynamics; flight modes; fractionated satellite system; hybrid modeling; hybrid system; logic rules; mixed logical dynamical approach; numerical simulations; power consumption; power management system; predictive control; Hybrid power systems; Imaging; Mathematical model; Predictive control; Predictive models; Satellites; Space vehicles; Fractionated satellite; Hybrid system; Mix logical dynamics; Modeling; Predictive control;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (CCDC), 2013 25th Chinese
Conference_Location
Guiyang
Print_ISBN
978-1-4673-5533-9
Type
conf
DOI
10.1109/CCDC.2013.6560920
Filename
6560920
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