共查询到20条相似文献,搜索用时 250 毫秒
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ANANALYSISOFPROPELLERLIFTING-LINETHEORYBYMATCHEDASYMPTOTICEXPANSIONSChenZemin;PanJieyuan;WuLiyi(InstituteofFluidMechanics,Bei... 相似文献
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Huang Mingke 《中国航空学报》1996,(1)
COMPUTATIONOFCOMPRESSIBLEFLOWPASTSLENDERWING-BODYUSINGFULL-POTENTIALEQUATIONHuangMingke(DepartmentofAerodynamics,NanjingUnive... 相似文献
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USEOFGENETICALGORITHMSTOSEQUENCETHEMACHININGOPERATIONSOFPARTSWANGXiyang(王细洋)(NanchangInstituteofAeronauticsTechnology,330034,... 相似文献
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Yuan Xiugan 《中国航空学报》1995,(3)
COMPUTERSIMULATIONINMAN-MACHINE-ENVIRONMENTSYSTEMENGINEERINGYuanXiugan(FifthDepartment,BeijingUniversityofAeronauticsandAstro... 相似文献
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WALLINTERFERENCECORRECTIONSFORHIGH-LIFTEXPERIMENTZhangWenhua(Faculty603ofNanjingUniversityofAeronauticsandAstronautics,Nanjin... 相似文献
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SIMPLIFYINGANDCONDENSINGASETOFRANDOMSPECTRAFORTRANSPORTZhangBaofa;FuXiangjiong(InstituteofStrength,NorthwesternPolytechnicalU... 相似文献
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CUTTINGTEMPERATUREOFCBNTOOLSWHENMACHININGSTEELOFMEDIUMHARDNESSChenWuyi1(陈五一),DavidK.Aspinwal2,HanShuwen3(韩书文)1BeijingUniversi... 相似文献
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SNAP-THROUGH OF LAMINATED ORTHOTROPIC SHALLOW SPHERICAL IMPERFECT SHELLS WITH TRANSVERSE SHEARYangYiqian;MaHezhong;WangTsunku... 相似文献
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Two important elements in the avionics suite of modern aircraft are: the flight control system (FCS) and the flight management system (FMS). The FCS provides the capability to stabilize and control the aircraft, while the FMS is responsible for flight planning and navigation. A clear trend in the aerospace industry is to place greater reliance on software systems, and many FCS and FMS subsystems are implemented primarily in software. For example, within the FCS is the flight guidance system (FGS) that generates roll and pitch guidance commands. Similarly, within the FMS is the vertical navigation (VNAV) function that acts like a third crew member in the cockpit, ordering mode change requests and resetting target altitude values to enable the aircraft to track the vertical flight plan. We have developed formal, executable models of the requirements for the mode logic of a FGS and for portions of the VNAV functionality. We have also conducted a comprehensive software safety analysis on the FGS mode logic model, and are completing the analysis of the VNAV model. This analysis uses as its starting point several "traditional" safety analysis techniques such as a functional hazard assessment (FHA), a fault tree analysis (FTA), and a failure mode effects analysis (FMEA). However, we are also using formal methods techniques known as model checking and theorem proving to verify the presence of safety properties in the model. This paper summarizes the (now completed) safety analysis that was performed on the FGS model, and highlights the similarities and differences with the (still on-going) safety analysis of the FMS model. In particular, we summarize progress made to date in the use of formal methods to verify the presence of the required safety properties in the models themselves. 相似文献
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把控制理论中的自适应控制策略应用到柔性制造系统仿真软件的开发中来,提出了自适应仿真思想用于柔性制造系统运行设计,在一定范围内解决了集成智能仿真环境中对柔性制造系统仿真结果的自动优化等问题,并对自适应仿真进行了展望。 相似文献
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The F-117A night attack aircraft flight management system (FMS) is described. The need for and purpose of the system are described, and the design goals are identified. The various modes and their important features are presented. The pitch and speed control laws are shown 相似文献
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基于FMS的Web视频、音频通信系统设计 总被引:1,自引:0,他引:1
针对目前流行的网络在线视频、音频通信的发展,研究了一种基于B/S结构下的Web视频、音频通信系统,并采用FMS技术、RTMP协议、AS语言等技术给予实现。从FMS的功能及采用的相关技术,所设计的系统对客户端、服务器的要求,设计的总体方法及核心技术的开发实现,系统的安全性及性能分析等方面进行阐述,并对系统的应用前景做了一定展望,希望能为下一代通信平台的构建提供较好的解决方案。 相似文献
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《Air & Space Europe》1999,1(1):42-44
Alternative Flight Management System (FMS) human interface concepts are becoming increasingly important to investigate as the complexities of understanding and operating this equipment continue to burden and confuse an already inundated pilot. Rockwell Collins, Inc. has designed an advanced FMS display/interface that will significantly reduce and/or eliminate human interface problems between users and the FMS. Results from human factors investigations for a limited set of FMS functions reveal statistically significant findings at the 95th level of confidence favoring the Advanced FMS Interface display format. The Advanced FMS Interface display format produced quicker reaction times and lower levels of mental workload than the a conventional Control Display Unit (CDU) type FMS.Furthermore, statistically significant findings at the 98th level of confidence for three subjective measures, Usability, Learnability, and Overall Attitude lean in favor of this type of FMS display format. These statistically significant findings lead us to believe that this Advanced FMS Interface display format has great potential for significantly reducing and/or eliminating human interface problems between users and the FMS while at the same time reducing pilot mental workload. 相似文献
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The requirements and design philosophy for developing ground-based automation planning and control advisory concepts to best serve aircraft with flight management systems (FMS) are defined. Analytical results are presented that are based on the comparison of operational data with the user-preferred trajectories to identify flying-time variabilities in various segments of arriving flights. En route descents, terminal maneuvering areas, and the final approaches are considered to determine the impact of aircraft and environmental factors on flying times essential for traffic planning. Simple time-estimation algorithms based on FMS-defined speed schedules and prevailing winds are presented for estimating flying times during en route descents. Automation, planning and control concepts are developed that utilize flexible route structures and a speed-control strategy to permit the aircraft maximum use of FMS and onboard avionics in all operating conditions 相似文献