• Title/Summary/Keyword: LEON2FT

Search Result 6, Processing Time 0.018 seconds

System Software Design and Simulation for LEON2-FT Processor based on PCI (PCI 기반 LEON2-FT 프로세서를 위한 시스템 소프트웨어 설계 및 시뮬레이션)

  • Choi, Jong-Wook;Nam, Byeong-Gyu
    • Journal of Satellite, Information and Communications
    • /
    • v.8 no.1
    • /
    • pp.54-60
    • /
    • 2013
  • The need for high performance of on-board computer (OBC) is essential due to the growing requirements and diversified missions, and so OBC has been developed on the basis of the standard design and reconfigurable modularization in order to improve the utilization of OBC for different missions. The processor in OBC of next generation satellite which is currently developed by KARI is adopted the LEON2-FT/AT697F processor based SPARC v8 as main processor and controls various devices such as SpaceWire, MIL-STD-1553B and CAN through PCI on the standardized communication chips. This paper presents the architecture and design of system software for LEON2-FT processor based on PCI, and development of PCI software component. Also it describes the porting of VxWorks 6.5 for LEON2-FT and the test under the simulation environment for LEON2-FT and PCI with communication chips.

Design and Implementation of a Processor Monitor and Fault Injection System for Next Generation Spacecraft Computer Board (차세대 위성탑재컴퓨터를 위한 프로세서 모니터 및 고장주입 시스템의 설계 및 구현)

  • Jeong, Jae-Yeop;Choi, Jong-Wook;Cheon, Yee-Jin
    • Journal of Satellite, Information and Communications
    • /
    • v.9 no.4
    • /
    • pp.97-103
    • /
    • 2014
  • In order to verify normal operation of satellite OBC(On Board Computer), it is essential that processor monitoring and debugging. So we are using the GRMON of Aeroflex Gaisler. It provides a lot of features for debugging of LEON processor but we can't use that features on the NGSCB(Next Generation Spacecraft Computer Board) except a few things. So the cost-effectiveness is very low. And for hardware fault injection, we are using a method of modify satellite flight software, because we can't modify GRMON. This method can not guarantee normal operation of the satellite flight software. So in this paper we were developed the processor monitoring and fault injection tool for NGSCB.

The effect of MedX exercise program on lumbar extensor strength in the elderly with chronic LBP (메덱스 척추강화운동 프로그램이 만성 요통 노인 환자들의 요부 신전 근력에 미치는 영향)

  • Cho, Hyun-Woo;Park, Sung-Kwang;Choi, Eun-Young;Kim, Myung-Joon
    • The Journal of Korean Academy of Orthopedic Manual Physical Therapy
    • /
    • v.10 no.2
    • /
    • pp.33-43
    • /
    • 2004
  • The purpose of this study was to compare the lumbar extensor strength between before exercise and after 8 weeks exercise in the elderly. To evaluate lumbar extensor strength of total 18 patients (above 59 age) with low back pain or have experienced surgical operation. Lumbar extensor strength was measured in 8 male patients and 10 female patients (9 op group and 9 non-op group) by Medx lumbar extension machine. The data were analyzed with paired t-test compared to muscle strength, with repeated measured ANOVA compared to amount increase of muscle strength, using SPSS ver. 10.0 program. The results of this study were as follows: 1. There were significantly increased total lumbar extension strength was appear $6918.7{\pm}2802.77$ft-lbs in before exercise, $10432.83{\pm}2802.773397.1$ft-lbs in after 8 weeks exercise (p<. 05). 2. There were significantly increased total lumbar extension strength was increased to compared before exercise with after 8 weeks exercise in sex (p<. 05), op/non-op group (p<. 05).

  • PDF

Design and Development of PCI-based 1553B Communication Software for Next Generation LEO On-Board Computer (차세대 저궤도 위성의 PCI 기반의 1553B 통신 소프트웨어 설계)

  • Choi, Jong-Wook;Jeong, Jae-Yeop;Yoo, Bum-Soo
    • Journal of Satellite, Information and Communications
    • /
    • v.11 no.3
    • /
    • pp.65-71
    • /
    • 2016
  • Currently developing the OBC of the next-generation LEO satellite by Korea Aerospace Research Institute adopts the LEON2-FT/AT697F processor to achieve high performance. And various communication devices such as SpaceWire, MIL-STD-1553B, DMAUART and CAN Master are integrated to the separated standard communication FPGAs within the OBC, where they can be controlled by the processor and flight software (FSW) through PCI interface. The Actel 1553BRM IP core is used for the 1553B in the next-generation LEO OBC and the B1553BRM wrapper from Aeroflex Gaisler is used for connecting it to the AMBA bus in FPGA. This paper presents the design and development of PCI-based 1553B communication software, and describes the handling mechanism of 1553B operation in FSW task level. Also it shows the test results on real-hardware and simulator.

Overhead Analysis of XtratuM for Space in SMP Envrionment (SMP 환경에서의 위성용 XtratuM 오버헤드 분석)

  • Kim, Sun-Wook;Yoo, Bum-Soo;Jeong, Jae-Yeop;Choi, Jong-Wook
    • IEMEK Journal of Embedded Systems and Applications
    • /
    • v.15 no.4
    • /
    • pp.177-187
    • /
    • 2020
  • Virtualization with hypervisors is one of emerging topics in multicore processors for space. Hypervisors are software layers to make several independent virtualized environments on one processor. Since all hardware resources are virtualized and distributed only by hypervisors, overall performance of processors can be improved by fully utilizing the resources. However at the same time, there are overheads for virtualizing and distributing hardware resources. Satellites are one of hard real time systems, and performance degradation with overheads should be analyzed thoroughly. Previous research on the overheads focused on single core systems. Even the overheads were analyzed in multicore systems, SMP environment was not fully included. This paper builds SMP environment with XtratuM, one of hypervisors for space missions, and analyzes performance degradation with overheads. Two boards of GR712RC with 2 LEON3FT CPUs and GR740 with 4 LEON4 CPUs are used in experiments. On each board, SMP benchmark functions are executed on SMP environment with XtratuM and on that without XtratuM respectively. Results are analyzed to find timing characteristics including overheads. Finally, applicability of the XtratuM to flight software in SMP is also reviewed.

Design and Implementation of OBCP Engine based on Lua VM for AT697F/VxWorks Platform (AT697F/VxWorks 플랫폼에서 Lua 가상머신 기반의 OBCP 엔진 설계 및 구현)

  • Choi, Jong-Wook;Park, Su-Hyun
    • Journal of Satellite, Information and Communications
    • /
    • v.12 no.3
    • /
    • pp.108-113
    • /
    • 2017
  • The OBCP called 'operator on board' is that of a procedure to be executed on-board, which can be easily be loaded, executed, and also replaced, without modifying the remainder of the FSW. The use of OBCP enhances the on-board autonomy capabilities and increases the robustness to ground stations outages. The OBCP engine which is the core module of OBCP component in the FSW interprets and executes of the procedures based on script language written using a high-level language, possibly compiled, and it is relying on a virtual machine of the OBCP engine. FSW team in KARI has studied OBCP since 2010 as FSW team's internal projects, and made some OBCP engines such as Java KVM, RTCS/C and KKOMA on ERC32 processor target only for study. Recently we have been studying ESA's OBCP standard and implementing Lua and MicroPython on LEON2-FT/AT697F processor target as the OBCP engine. This paper presents the design and implementation of Lua for the OBCP engine on AT697F processor with VxWorks RTOS, and describes the evaluation result and performance of the OBCP engine.