DocumentCode
558853
Title
Spacecraft dynamics and control simulation system based on LabVIEW software
Author
Jin, Jaehyun
Author_Institution
Dept. of Aerosp. Eng., Sunchon Nat. Univ., Sunchon, South Korea
fYear
2011
fDate
26-29 Oct. 2011
Firstpage
1888
Lastpage
1890
Abstract
The author introduces a simulation system for spacecraft dynamics and control developed by LabVIEW program. The system has a function to interface with hardware. A variable-speed CMG has been considered as an actuator. Sensors such as a magnetic compass and gyros are adopted. This simulation system has been developed for the purpose of education and research. Systems engineering process also has been used to design the system.
Keywords
actuators; aerospace computing; aerospace instrumentation; aircraft control; compasses; gyroscopes; sensors; space vehicles; systems engineering; velocity control; virtual instrumentation; LabVIEW software; actuator; education; magnetic compass; sensor; spacecraft control simulation system; spacecraft dynamics; system design; systems engineering process; variable-speed control moment gyroscope; Adaptation models; Aerodynamics; Mathematical model; Modeling; Satellites; Sensors; Space vehicles; LabVIEW program; PILS system; Simulation system; Systems Engineering; Variable-speed CMG;
fLanguage
English
Publisher
ieee
Conference_Titel
Control, Automation and Systems (ICCAS), 2011 11th International Conference on
Conference_Location
Gyeonggi-do
ISSN
2093-7121
Print_ISBN
978-1-4577-0835-0
Type
conf
Filename
6106187
Link To Document