2010 IEEE Aerospace Conference最新文献_第8页

Delay/Disruption-Tolerant Networking: Flight test results from the international space station 延迟/容错网络:来自国际空间站的飞行测试结果

2010 IEEE Aerospace Conference Pub Date : 2010-03-06 DOI: 10.1109/AERO.2010.5446948

Andrew Jenkins, Sebastian Kuzminsky, Kevin K. Gifford, R. Pitts, Kelvin Nichols

引用次数: 57

On the optimization of DVB-S2 links in EHF bands EHF频段DVB-S2链路优化研究

2010 IEEE Aerospace Conference Pub Date : 2010-03-06 DOI: 10.1109/AERO.2010.5446998

S. Mukherjee, M. De Sanctis, T. Rossi, E. Cianca, M. Ruggieri, R. Prasad

引用次数: 16

Removing spikes while preserving data and noise using wavelet filter banks 去除尖峰，同时保留数据和噪声使用小波滤波器组

2010 IEEE Aerospace Conference Pub Date : 2010-03-06 DOI: 10.1109/AERO.2010.5446821

E. Sheybani, O. Mengshoel, S. Poll

引用次数: 19

Human rated Delta IV Heavy Constellation architecture impacts 人类评级德尔塔IV重型星座建筑影响

2010 IEEE Aerospace Conference Pub Date : 2010-03-06 DOI: 10.1109/AERO.2010.5446891

M. Hart, D. Bearden, J. Skratt

引用次数: 4

Field test implementation to evaluate a flash LIDAR as a primary sensor for safe lunar landing 实地测试实施，评估闪光激光雷达作为安全登月的主要传感器

2010 IEEE Aerospace Conference Pub Date : 2010-03-06 DOI: 10.1109/AERO.2010.5447024

J. Keim, S. Mobasser, D. Kuang, Yang Cheng, Tonislav Ivanov, Andrew E. Johnson, H. Goldberg, G. Khanoyan, D. Natzic

引用次数: 26

A new analytical model of a radial turbine and validation by experiments 一种新的径向水轮机解析模型及实验验证

2010 IEEE Aerospace Conference Pub Date : 2010-03-06 DOI: 10.1109/AERO.2010.5446764

H. Pourfarzaneh, A. Hajilouy-Benisi, M. Farshchi

{"title":"A new analytical model of a radial turbine and validation by experiments","authors":"H. Pourfarzaneh, A. Hajilouy-Benisi, M. Farshchi","doi":"10.1109/AERO.2010.5446764","DOIUrl":"https://doi.org/10.1109/AERO.2010.5446764","url":null,"abstract":"In the conceptual design phase of a turbocharger, where emphasis is mainly on parametric studies, before manufacturing and tests, a generalized and robust model that applies over a wide range properly, is unavoidable. 12The critical inputs such as turbine maps are not available during the conceptual design phase. Hence, generalized turbine models use alternate methods that work without any supplementary tests and can operate over wide ranges. One of the common and applicable modeling methods in design process is ‘Dimensionless Modeling’ using the constant coefficient scaling (CCS). This method can almost predict the turbine characteristics at the design point. However, at off-design conditions, the error goes up as mass flow and speed parameters increase. Therefore, the results are not reliable at these points. In this paper, a variable coefficient scaling (VCS) method is described. Then, a radial turbine is modeled using the VCS method. To evaluate the model and compare it with the experimental results, some supplementary experiments are performed. Experimental studies are carried out on the turbine of a S2B model of the Schwitzer turbocharger in the turbocharger Lab., at Sharif University of Technology. The comparison between the experimental results and those obtained by the VCS method indicates good agreement. It also suggests that the present model can be used as an effective design tool for all operating conditions.","PeriodicalId":378029,"journal":{"name":"2010 IEEE Aerospace Conference","volume":"67 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2010-03-06","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114138324","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 2

Hub and Spoke BGP: Leveraging multicast to improve wireless inter-domain routing Hub and Spoke BGP:利用组播来改进无线域间路由

2010 IEEE Aerospace Conference Pub Date : 2010-03-06 DOI: 10.1109/AERO.2010.5446936

Joshua Train, B. Etefia, Harley Green

引用次数: 7

Markov analysis of human-in-the-loop system performance 人在环系统性能的马尔可夫分析

2010 IEEE Aerospace Conference Pub Date : 2010-03-06 DOI: 10.1109/AERO.2010.5446860

S. Bortolami, K. Duda, N. Borer

{"title":"Markov analysis of human-in-the-loop system performance","authors":"S. Bortolami, K. Duda, N. Borer","doi":"10.1109/AERO.2010.5446860","DOIUrl":"https://doi.org/10.1109/AERO.2010.5446860","url":null,"abstract":"Pilot interaction with complex vehicles involves information perception and understanding, as well as decision making to select and execute the desired action. These decisions and actions are often time-critical and require an accurate response. When designing a complex system, the analysis of human-in-the-loop system performance is important during early-stage system design to assess the impact of varying levels of automation, redundancy, and task allocation. We have integrated several human performance models with a model of a piloted vehicle to analyze human-in-the-loop performance using Draper Laboratory's Performance and Reliability Analysis via Dynamic Modeling (PARADyM) toolkit. This approach provides a framework for understanding the effects of a vehicle component failure or human error as it propagates through a complex system. Vehicle and human performance models, which include a model of the Space Shuttle Orbiter lateral flight dynamics, visual and vestibular perception, rule-based judgment and decision making, and pilot action, were implemented using MATLAB/Simulink?. Trajectory scenarios were simulated for analysis with and without instrumentation failures, and with and without human errors. The resulting pilot-vehicle performance during scenarios with a component failure was compared to a baseline (no failure) trajectory. Performance thresholds were specified to determine whether the resulting vehicle trajectory represented degraded performance that was within the specified bounds (operational) or outside the bounds (resulting in system loss). At the present stage, this analysis methodology is viable as an early-stage design tool. However, if associated with experimentally validated models for both the human performance and vehicle dynamics, this approach has the potential for a mission and configuration design analysis tool.","PeriodicalId":378029,"journal":{"name":"2010 IEEE Aerospace Conference","volume":"143 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2010-03-06","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116047249","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 13

A 320 Mbps flexible image data compressor for space applications 用于空间应用的320mbps灵活图像数据压缩器

2010 IEEE Aerospace Conference Pub Date : 2010-03-06 DOI: 10.1109/AERO.2010.5446664

P. Winterrowd, Chad Orbe, J. Venbrux, S. Whitaker, E. Cameron, R. Nelson, G. Maki, D. Fisher, P. Yeh

引用次数: 15

Application of hierarchical accident model in independent verification and validation 分层事故模型在独立验证中的应用

2010 IEEE Aerospace Conference Pub Date : 2010-03-06 DOI: 10.1109/AERO.2010.5446810

R. Ujiie, M. Katahira, Tsutomu Matsumoto, A. Katoh, Shogo Ujihara

引用次数: 2