Abstract
The design of spacecraft attitude control is important during the manufacture of spacecraft, and it is need to be validated adequately. To get the digital simulation validation of attitude control system, this paper discussed the spacecraft attitude control simulation system based on STK, Matlab and ADAMS. Based on the simulation frame, the paper analyzed the simulation model inter-clock. and realized the simulation system clock synchronization mechanism and algorithm. Based on the method of clock synchronization, the clock synchronization and logic correctness of message among multi-disciplinary simulation models could be ensured.
Full Text 
Sign-in/Register to access full text options
Sign-in/Register to access full text options 
Paper version not known
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a call
