DocumentCode
2728017
Title
Consensus-based controllers for spacecraft attitude alignment: Simulation results
Author
Septanto, Harry ; Riyanto-Trilaksono, Bambang ; Syaichu-Rohman, Arief ; Eko-Poetro, Ridanto
Author_Institution
Scool of Electr. Eng. & Inf., Inst. Teknol. Bandung, Bandung, Indonesia
fYear
2011
fDate
8-9 Nov. 2011
Firstpage
52
Lastpage
57
Abstract
Spacecraft formation flying control using consensus algorithm means each spacecraft or satellite in a team updates its state based on the information states of its local neighbours in such a way that the final information state of each agent converges to a common value. This paper discusses spacecraft formation within scope of rotational motions i.e. attitude alignment. Two attitude alignment controllers based on consensus algorithm proposed here.Simulations that run as preliminary proof a concept are presented. Simulations run indicate the proposed control laws might solve the attitude alignment problem i.e. consensus is achieved.
Keywords
attitude control; motion control; space vehicles; attitude alignment; consensus based controllers; control laws; rotational motions; satellite; spacecraft attitude alignment; spacecraft formation flying control; Angular velocity; Attitude control; Biomedical engineering; Instruments; Mathematical model; Space vehicles; Topology; Spacecraft formation flying; attitude alignment; consensus algorithm; nonlinear control system; simulation;
fLanguage
English
Publisher
ieee
Conference_Titel
Instrumentation, Communications, Information Technology, and Biomedical Engineering (ICICI-BME), 2011 2nd International Conference on
Conference_Location
Bandung
Print_ISBN
978-1-4577-1167-1
Type
conf
DOI
10.1109/ICICI-BME.2011.6108593
Filename
6108593
Link To Document