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논문 기본 정보

자료유형
학술저널
저자정보
Won Seop Choe (Pusan National University) Dong In Han (Pusan National University) Chan Oh Min (Pusan National University) Sang Man Kim (Pusan National University) Young Sik Kim (Pusan National University) Dae Woo Lee (Pusan National University)
저널정보
한국항공우주학회 International Journal of Aeronautical and Space Sciences International Journal of Aeronautical and Space Sciences Volume.18 Number.4
발행연도
2017.12
수록면
675 - 687 (13page)
DOI
10.5139/IJASS.2017.18.4.675

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초록· 키워드

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In the aerospace industry, we have produced various models according to operational conditions and the environment after development of the base model is completed. Therefore, when design change is necessary, there are modification and updating costs of the circuit whenever environment variables change. For these reasons, recently, in various fields, system designs that can flexibly respond to changing environmental conditions using field programmable gate arrays (FPGAs) are attracting attention, and the rapidly changing aerospace industry also uses FPGAs to organize the system environment. In this paper, we design the controller area network (CAN) intellectual property (IP) protocol used instead of the avionics protocol that includes ARINC-429 and MIL-STD-1553, which are not suitable for small unmanned aerial vehicle (UAV) systems at the register transistor logic (RTL) level, which does not depend on the FPGA vender, and we verify the performance. Consequentially, a Spartan 6 FPGA model–based system on chip (SoC) including an embedded system is constructed by using the designed CAN communications IP and Xilinx Microblaze, and the configured SoC only recorded an average 32% logic element usage rate in the Spartan 6 FPGA model.

목차

Abstract
1. Introduction
2. IP configuration
3. Experimental results
4. SoC configuration
5. Conclusion
References

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