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82.
基于支持向量机的航空发动机辨识模型 总被引:4,自引:3,他引:4
针对航空发动机具有强非线性、时变性的特点以及采用常规神经网络辨识时存在的局部较小,过学习等问题,提出了一种基于支持向量机的通用发动机模型辨识方法。该方法基于现代统计学习理论,采用结构风险最小化准则,保证了网络具有很强的推广特性,通过求解凸二次规划确保网络结构全局最优化自动生成。本文采用实测到的发动机飞行记录数据作为训练样本,利用回归型支持向量机建立了发动机的辨识模型,研究结果表明该方法的辨识精度较高,鲁棒性、容错性较好,具有较大的实用价值。 相似文献
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84.
Flavio S. Correa da Silv Marcelo K. Zuffo Paul W. H. Chung Petros Papapanagiotou David Robertson 《民用飞机设计与研究》2017,(3):105
Hazard prevention in mission plans requires careful analysis and appropriate tools to support the design of preventive and/or corrective measures. It is most challenging in systems with large sets of states and complex state relations. In the case of sociotechnical systems, hazard prevention becomes even more dicult given that the behaviour of human centric components can at best be partially predictable. In the present article we focus on a specic class of sociotechnical systems namely air spaces containing pilot controlled as well as autonomous aircrafts and introduce the notion of relevant hazards. We also introduce soft institutions as an appropriate basis for analysis, with the aim of addressing relevant hazards. The concept of soft institutions is drawn from specication languages for interaction between agents in multi agent systems but, in our case, is adapted for use in systems that combine human and automated actors. 相似文献
85.
《中国航空学报》2020,33(7):1980-1990
Uncontained Engine Rotor Failure (UERF) can cause a catastrophic failure of an aircraft, and the quantitative assessment of the hazards related to UERF is a very important part of safety analysis. However, the procedure for hazard quantification of UERF recommended by the Federal Aviation Administration in advisory circular AC20-128A is cumbersome, as it involves building auxiliary lines and curve projections. To improve the efficiency and general applicability of the risk angle calculation, a boundary discretization method is developed that involves discretizing the geometry of the target part/structure into node points and calculating the risk angles numerically by iterating a particular algorithm over each node point. The improved efficiency and excellent accuracy for the developed algorithm was validated through a comparison with manual solutions for the hazard quantification of the engine nacelle structures of a passenger aircraft using the guidance in AC20-128A. To further demonstrate the applicability of the boundary discretization method, the proposed algorithm was used to examine the influence of the target size and the distance between the target and rotor on the hazard probability. 相似文献
86.
Althea V. Moorhead Mark Matney 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(1):384-392
Orbital debris is known to pose a substantial threat to Earth-orbiting spacecraft at certain altitudes. For instance, the orbital debris flux near Sun-synchronous altitudes of 600–800 km is particularly high due in part to the 2007 Fengyun-1C anti-satellite test and the 2009 Iridium-Kosmos collision. At other altitudes, however, the orbital debris population is minimal and the primary impactor population is not man-made debris particles but naturally occurring meteoroids. While the spacecraft community has some awareness of the risk posed by debris, there is a common misconception that orbital debris impacts dominate the risk at all locations. In this paper, we present a damage-limited comparison between meteoroids and orbital debris near the Earth for a range of orbital altitude and inclination, using NASA’s latest models for each environment. Overall, orbital debris dominates the impact risk between altitudes of 600 and 1300 km, while meteoroids dominate below 270 km and above 4800 km. 相似文献
87.
Software defect prevention is an important way to reduce the defect introduction rate.As the primary cause of software defects,human error can be the key to understanding and preventing software defects.This paper proposes a defect prevention approach based on human error mechanisms:DPeHE.The approach includes both knowledge and regulation training in human error prevention.Knowledge training provides programmers with explicit knowledge on why programmers commit errors,what kinds of errors tend to be committed under different circumstances,and how these errors can be prevented.Regulation training further helps programmers to promote the awareness and ability to prevent human errors through practice.The practice is facilitated by a problem solving checklist and a root cause identification checklist.This paper provides a systematic framework that integrates knowledge across disciplines,e.g.,cognitive science,software psychology and software engineering to defend against human errors in software development.Furthermore,we applied this approach in an international company at CMM Level 5 and a software development institution at CMM Level 1 in the Chinese Aviation Industry.The application cases show that the approach is feasible and effective in promoting developers' ability to prevent software defects,inde pendent of process maturity levels. 相似文献
88.
某型飞机装有两套HZX-1航向姿态系统,飞行中同时出现转弯航向误差大现象,本文通过分析故障原因,找出了引起故障的关键产品,并针对故障制定了预防措施。 相似文献
89.
张建桥 《郑州航空工业管理学院学报(管理科学版)》2011,29(1)
预防和治理城市病,要顺应城市化趋势,贯彻人本理念,加强战略谋划和长远规划,努力增加大城市数量,促进各城市平衡发展;科学规划城市建设,扩大公共服务供给;加强城市公用设施建设,大力提高市民的规则意识和城市领导者的组织治理能力。 相似文献
90.
Siwoo Kim Byeong-Un Jo Eun-Jung Choi Sungki Cho Jaemyung Ahn 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(6):1844-1858
This paper proposes a procedure for managing the risk of reentering space objects and risk assessment methodologies used for the process. The proposed procedure comprises three phases encompassing the whole reentry stages of space objects. Mathematical models for assessing the impact risk of the reentering space objects by utilizing the information available during different risk management phases and the recommended risk analysis results for public communication are presented. The concept of the conditional casualty expectation is proposed as the metric representing the reentry risk and the method to compute its profile is introduced. A case study on the risk management procedure with the dataset on an actual reentry event is conducted to demonstrate the efficacy of the proposed procedure. 相似文献