DocumentCode
3272931
Title
Research on algorithms of land-to-air missile launch control system based on CAN bus
Author
Jiang Zhi-peng ; Han Hua-ting ; Feng Gang ; Dai Xin-sheng
Author_Institution
Missile Inst., Air Force Eng. Univ., Sanyuan, China
fYear
2011
fDate
15-17 April 2011
Firstpage
2501
Lastpage
2503
Abstract
In terms of the characteristics of CAN bus in the launch control system and the messages transmitted in network, a scheduling algorithm which is combined with Deadline Monotonic and Distributed Priority Queue scheduling algorithm is presented. The method is based on the CAN bus´s rule of priority´s arbitration bit by bit without destroy. Finally, the tracking simulation is carried out on the MATLAB platform, results show that it improves the transmission efficiency of CAN bus.
Keywords
control engineering computing; controller area networks; missile control; queueing theory; scheduling; CAN bus; MATLAB platform; deadline monotonic algorithm; distributed priority queue scheduling algorithm; land-to-air missile launch control system; tracking simulation; transmission efficiency; Control systems; Delta modulation; Missiles; Real time systems; Scheduling; Scheduling algorithm; Time factors; CAN bus; DPQ; launch control system;
fLanguage
English
Publisher
ieee
Conference_Titel
Electric Information and Control Engineering (ICEICE), 2011 International Conference on
Conference_Location
Wuhan
Print_ISBN
978-1-4244-8036-4
Type
conf
DOI
10.1109/ICEICE.2011.5777239
Filename
5777239
Link To Document