DocumentCode
2670965
Title
Research and simulation on space mobile platform mission on orbit
Author
Baiwei, Guo ; Jiuhui, Ding
Author_Institution
Key Lab. of Dynamics & Control of Flight Vehicle, Beijing Inst. of Technol., Beijing, China
fYear
2012
fDate
23-25 May 2012
Firstpage
2158
Lastpage
2161
Abstract
For on-orbit service characteristics of one class of space mobile platform, this paper make a simulation on the orbit and attitude maneuver, design and analysis the theory and performance of the ATP(Acquisition, Tracking, Pointing) system, and build one space mobile platform simulation system in java based on PRTI and HLA(High Level Architecture). The simulation system can verify the effectiveness of platform maneuver strategy and ATP.
Keywords
Java; aerospace computing; celestial mechanics; high level synthesis; space vehicles; ATP system; HLA; Java; PRTI; acquisition-tracking-pointing system; attitude maneuver strategy; high level architecture; on-orbit service characteristic; space mobile platform mission simulation system; Acceleration; Aerospace electronics; Mathematical model; Mobile communication; Orbits; Space vehicles; Tracking loops; ATP; HLA; Orbit and attitude maneuver; Space mobile platform;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (CCDC), 2012 24th Chinese
Conference_Location
Taiyuan
Print_ISBN
978-1-4577-2073-4
Type
conf
DOI
10.1109/CCDC.2012.6244346
Filename
6244346
Link To Document