Title :
Hardware-in-loop simulation analysis of spacecraft attitude control system
Author :
Qi, Zheng ; Pan, Feng ; Hu, Song
Author_Institution :
Sch. of Astronaut., Beihang Univ., Beijing, China
Abstract :
In the paper, to simplify the measurement and attitude control system, the simulation equipment is proposed. The soft simulation is simplified by substituting the virtual model with hardware-in-loop simulation. Meanwhile, a process transforms the three-dimension movement to two-dimension movement, and realizes simulation on uniaxial simulation equipment. A model in MATLAB/Simulink is done to compare the result of uniaxial simulation equipment. The result indicates that the uniaxial simulation equipment is feasible and accurate, and can be used in testing control algorithm.
Keywords :
aerospace computing; aircraft control; attitude control; digital simulation; measurement systems; space vehicles; MATLAB; Simulink; hardware-in-loop simulation analysis; measurement system; soft simulation; spacecraft attitude control system; testing control algorithm; three-dimension movement; two-dimension movement; uniaxial simulation equipment; virtual model; Attitude control; Blades; Control systems; Equations; Force; Mathematical model; Space vehicles; PID; hardware-in-loop simulation; release payload; system control;
Conference_Titel :
Artificial Intelligence, Management Science and Electronic Commerce (AIMSEC), 2011 2nd International Conference on
Conference_Location :
Deng Leng
Print_ISBN :
978-1-4577-0535-9
DOI :
10.1109/AIMSEC.2011.6010777
