DocumentCode
234977
Title
Information Flow Control Model and Method in Distribute MILS
Author
Kaiqiang Li ; Hao Feng ; Yahui Li ; Zhiwei Zhang
Author_Institution
Sch. of Comput. Sci. & Technol., Xidian Univ., Xi´an, China
fYear
2014
fDate
15-16 Nov. 2014
Firstpage
598
Lastpage
602
Abstract
A new generation of avionics system has three major technical characteristics of high resource sharing, data integration and software intensive. However, in the cooperative combat environment, which has the problem of potential sensitive information leakage and tamper when the combat aircraft communicate with each other. In this paper, we are based on the single node of information flow control model, combined with PCS, proposed a distributed information flow control model in MILS, constructed the PCS information flow control strategy, and together with other trusted component of information flow control strategy that form the multi-level information flow control policy framework, which design an information flow control mechanism of PCS and realized the distributed information flow control in MILS. After analysis and verification, the design of the distributed information flow security control method in MILS can effectively ensure the confidentiality and integrity of the information among the nodes.
Keywords
avionics; information dissemination; security of data; MILS; avionics system generation; cooperative combat environment; data integration; high resource sharing; information flow control model; multilevel information flow control policy framework; multiple independent levels of security; potential sensitive information leakage; software intensive; Aerospace electronics; Encryption; Kernel; Middleware; Ports (Computers); distribute; information flow control; mils; pcs; security policy;
fLanguage
English
Publisher
ieee
Conference_Titel
Computational Intelligence and Security (CIS), 2014 Tenth International Conference on
Conference_Location
Kunming
Print_ISBN
978-1-4799-7433-7
Type
conf
DOI
10.1109/CIS.2014.48
Filename
7016966
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