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Single event upset(SEU)effect,caused by highly energized particles in aerospace,threatens the reliability and security of small satellites composed of commercial-off-the-shelves(COTS).SEUinduced control flow errors(CFEs)may cause unpredictable behavior or crashes of COTS-based small satellites.This paper proposes a generic software-based control flow checking technique(CFC)and bipartite graph-based control flow checking(BGCFC).To simplify the types of illegal branches,it transforms the conventional control flow graph into the equivalent bipartite graph.It checks the legality of control flow at runtime by comparing a global signature with the expected value and introduces consecutive IDs and bitmaps to reduce the time and memory overhead.Theoretical analysis shows that BGCFC can detect all types of inter-node CFEs with constant time and memory overhead.Practical tests verify the result of theoretical analysis.Compared with previous techniques,BGCFC achieves the highest error detection rate,lower time and memory overhead;the composite result in evaluation factor shows that BGCFC is the most effective one among all these techniques.The results in both theory and practice verify the applicability of BGCFC for COTS-based small satellites. 相似文献
474.
This paper presents comparative numerical studies to investigate the effects of blade sweep on inlet flow in axial compressor cascades. A series of swept and straight cascades was modeled in order to obtain a general understanding of the inlet flow field that is induced by sweep.A computational fluid dynamics(CFD) package was used to simulate the cascades and obtain the required three-dimensional(3D) flow parameters. A circumferentially averaged method was introduced which provided the circumferential fluctuation(CF) terms in the momentum equation.A program for data reduction was conducted to obtain a circumferentially averaged flow field.The influences of the inlet flow fields of the cascades were studied and spanwise distributions of each term in the momentum equation were analyzed. The results indicate that blade sweep does affect inlet radial equilibrium. The characteristic of radial fluid transfer is changed and thus influencing the axial velocity distributions. The inlet flow field varies mainly due to the combined effect of the radial pressure gradient and the CF component. The axial velocity varies consistently with the incidence variation induced by the sweep, as observed in the previous literature. In addition, factors that might influence the radial equilibrium such as blade camber angles, solidity and the effect of the distance from the leading edge are also taken into consideration and comparatively analyzed. 相似文献
475.
Survey of orbital dynamics and control of space rendezvous 总被引:2,自引:1,他引:1
Rendezvous orbital dynamics and control (RODC) is a key technology for operating space rendezvous and docking missions. This paper surveys the studies on RODC. Firstly, the basic relative dynamics equation set is introduced and its improved versions are evaluated. Secondly, studies on rendezvous trajectory optimization are commented from three aspects: the linear rendez- vous, the nonlinear two-body rendezvous, and the perturbed and constrained rendezvous. Thirdly, studies on relative navigation are briefly reviewed, and then close-range control methods including automated control, manual control, and telecontrol are analyzed. Fourthly, advances in rendezvous trajectory safety and robust analysis are surveyed, and their applications in trajectory optimization are discussed. Finally, conclusions are drawn and prospects of studies on RODC are presented. 相似文献
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477.
针对领域本体维护的重要性与合并本体存在的异构本体及不一致性错误等问题,提出了一种基于本体合并的领域本体自动维护方法,对相关实现过程作了详细介绍,重点给出了概念的相似性匹配算法.该算法通过计算概念的定义、实例、属性、关系及推理的相似度,得到了本体中概念之间的相似度.本文还探讨了本体不一致性的错误,分析了概念间的上下位关系、非通用关系及相关特性的不一致,并给出了解决方案.实验结果表明,该方法具有一定的实用性和可靠性,能够得到较正确的领域本体的维护结果,并能够解决相关不一致的错误. 相似文献
478.
金童 《民用飞机设计与研究》2011,(4):72-74
随着计算机和网络技术的普及和发展,相应产生的大量电子文件正在给我们的工作和生活带来巨大的变化,它与纸质文件的归档和管理截然不同,给传统的档案管理工作带来了严峻的挑战,我们迫切需要对电子文件的归档和归档后的电子档案进行规范、科学地管理。 相似文献
479.
480.
JIN Weiqing Shinichi Yoda Jiang Yuanfang LIANG Xinan PAN Zhilei Shen Guotu Liu Zhaohua 《空间科学学报》2002,22(Z1)
We have investigated experimentally and theoretically the thermocapillary convec tive flow phenomena in a loop-shaped Pt wire heater of KNbO3 (20wt.%) and Li2B4O7 solutions. Optical evaluations in connection with thermocouple measure ments made it possible to get a new type of thermocapillary convective flow in the considered system. To study the kinematical behaviour of thermocapillary convec tion, we have measured the stream flow velocities. In a theoretical analysis, the flow velocity due to the thermocapillary effect alone was estimated by balancing the sur face tension forces by viscous forces. The velocity distribution in the solution near the margin of the heater was obtained, which is in agreement with the experimental result. 相似文献