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2018 Modeling and Simulation Technologies Conference最新文献

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New Economical Cruise Methodology for the Cessna Citation X Business Jet by an Original Morphing Horizontal Tail Application 基于原始变形水平尾翼应用的塞斯纳引文X公务机新经济巡航方法
2018 Modeling and Simulation Technologies Conference Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3895
M. Segui, M. Mantilla, Georges Ghazi, R. Botez
{"title":"New Economical Cruise Methodology for the Cessna Citation X Business Jet by an Original Morphing Horizontal Tail Application","authors":"M. Segui, M. Mantilla, Georges Ghazi, R. Botez","doi":"10.2514/6.2018-3895","DOIUrl":"https://doi.org/10.2514/6.2018-3895","url":null,"abstract":"","PeriodicalId":326346,"journal":{"name":"2018 Modeling and Simulation Technologies Conference","volume":"15 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129613798","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: 5
Withdrawal: A Novel Method to Build a Factor Space for Model Validation 撤回:一种建立模型验证因子空间的新方法
2018 Modeling and Simulation Technologies Conference Pub Date : 2018-06-24 DOI: 10.1007/978-981-13-2853-4_1
K. Fang, Ming Yang, Yuchen Zhou
{"title":"Withdrawal: A Novel Method to Build a Factor Space for Model Validation","authors":"K. Fang, Ming Yang, Yuchen Zhou","doi":"10.1007/978-981-13-2853-4_1","DOIUrl":"https://doi.org/10.1007/978-981-13-2853-4_1","url":null,"abstract":"","PeriodicalId":326346,"journal":{"name":"2018 Modeling and Simulation Technologies Conference","volume":"64 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126552484","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
Generic Control Allocation Toolbox for Preliminary Vehicle Design 车辆初步设计通用控制分配工具箱
2018 Modeling and Simulation Technologies Conference Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3894
Jing Pei, G. Bassett, J. Grisham, P. Finch, Matthew D. Toniolo, Luke J. Miller, Pamadi Bandu
{"title":"Generic Control Allocation Toolbox for Preliminary Vehicle Design","authors":"Jing Pei, G. Bassett, J. Grisham, P. Finch, Matthew D. Toniolo, Luke J. Miller, Pamadi Bandu","doi":"10.2514/6.2018-3894","DOIUrl":"https://doi.org/10.2514/6.2018-3894","url":null,"abstract":"This paper describes the development and application of a Generic Control Allocation Toolbox developed at NASA Langley Research Center (LGCAT) intended to aid engineers during the preliminary design phase of an aerospace vehicle. The static controllability space in the forms of a Theoretical Attainable Moment Set, Φ, or Theoretical Attainable Force Set, φ is difficult to visualize for modern vehicles with multiple types of redundant control effectors. The objective of LGCAT is to provide system engineers and designers early in the vehicle design phase with quick insights on how control effector parameters such as quantity, sizing, location, orientation, redundancy, etc., affect the overall controllability and other performance metrics. Having such information in hand allows system engineers to make more informed decisions on overall mission objectives such as performance vs. reliability vs. cost, etc. early in a vehicle design phase and reduce the number of iterations necessary in the design and analysis cycles. LGCAT can accept a variety of control effector types including aerodynamic surfaces, rotors, thrust vector control (TVC) engines, and reaction control systems (RCS). LGCAT is MATLAB based, user friendly, and is capable of performing the analysis in the Graphical User Interface (GUI) or script mode. Current add-on features include interfacing with engineering level codes such as Vehicle Sketch Pad (VSP) and generating the corresponding Φ and φ for an arbitrary vehicle design. These capabilities potentially make LGCAT an integral part of the preliminary design phase for any vehicle.","PeriodicalId":326346,"journal":{"name":"2018 Modeling and Simulation Technologies Conference","volume":"20 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114068466","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
Evaluation of Augmented Reality Tools for the provision of Tower Air Traffic Control using An Ecological Interface Design 利用生态界面设计对提供塔台空中交通管制的增强现实工具进行评估
2018 Modeling and Simulation Technologies Conference Pub Date : 2018-06-24 DOI: 10.2514/6.2018-2939
M. Ellejmi, S. Bagassi, A. Persiani
{"title":"Evaluation of Augmented Reality Tools for the provision of Tower Air Traffic Control using An Ecological Interface Design","authors":"M. Ellejmi, S. Bagassi, A. Persiani","doi":"10.2514/6.2018-2939","DOIUrl":"https://doi.org/10.2514/6.2018-2939","url":null,"abstract":"One of the major problems faced by the growth of air traffic in the last decade is the limited capacity of the runway especially during low visibility procedures (LVP) due to fog and bad weather. To solve this issue, the project “Resilient Synthetic Vision for Advanced Control Tower Air Navigation Service Provision” (RETINA) project, a two-years exploratory research project, under SESAR2020 program, proposes to use new Synthetic Vision (SV) and Augmented Reality (AR) technologies for the tower controllers to allow them to conduct safe operations under any Meteorological Conditions while maintaining a high runway throughput, equal to good visibility. In this paper we introduce the Ecological Interface Design (EID) as a methodology to investigate the potential and applicability of SV tools and Virtual/Augmented Reality (V/AR) display techniques for the Air Traffic Control (ATC) service provision by the airport control tower. We explain how the EID framework can be used in RETINA, we experiment the framework on a suitable airport and we provide the EID results comparing normal and LVP conditions with operations using RETINA technologies.","PeriodicalId":326346,"journal":{"name":"2018 Modeling and Simulation Technologies Conference","volume":"326 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"115872111","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: 7
A computational interface for Steady-State Models: An FMI Extension 稳态模型的计算接口:一种FMI扩展
2018 Modeling and Simulation Technologies Conference Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3893
Giulio M. Mancuso, Fabio Cremona, L. Mangeruca, A. Ulisse, Alessandro Mignogna, Stefano Boccabella, A. Ferrari, L. D. Guglielmo
{"title":"A computational interface for Steady-State Models: An FMI Extension","authors":"Giulio M. Mancuso, Fabio Cremona, L. Mangeruca, A. Ulisse, Alessandro Mignogna, Stefano Boccabella, A. Ferrari, L. D. Guglielmo","doi":"10.2514/6.2018-3893","DOIUrl":"https://doi.org/10.2514/6.2018-3893","url":null,"abstract":"","PeriodicalId":326346,"journal":{"name":"2018 Modeling and Simulation Technologies Conference","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130775014","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: 1
Human-in-the-Loop Study on Angle-of-Attack Indicator Effectiveness for Transport Category Airplanes 运输机迎角指示器有效性的人在环研究
2018 Modeling and Simulation Technologies Conference Pub Date : 2018-06-24 DOI: 10.2514/6.2018-2938
A. Campbell, Somil R. Shah, M. Reisweber, L. L. Vie
{"title":"Human-in-the-Loop Study on Angle-of-Attack Indicator Effectiveness for Transport Category Airplanes","authors":"A. Campbell, Somil R. Shah, M. Reisweber, L. L. Vie","doi":"10.2514/6.2018-2938","DOIUrl":"https://doi.org/10.2514/6.2018-2938","url":null,"abstract":"","PeriodicalId":326346,"journal":{"name":"2018 Modeling and Simulation Technologies Conference","volume":"24 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132894161","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: 1
Characterizing Effects of Aircraft Dynamics on Airborne Antenna Arrays by Generating In-Flight Deformed Geometry for Finite Element Analysis 飞机动力学对机载天线阵列影响的有限元分析
2018 Modeling and Simulation Technologies Conference Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3584
Pedro Martin Mendoza Strilchuk, E. Arnold
{"title":"Characterizing Effects of Aircraft Dynamics on Airborne Antenna Arrays by Generating In-Flight Deformed Geometry for Finite Element Analysis","authors":"Pedro Martin Mendoza Strilchuk, E. Arnold","doi":"10.2514/6.2018-3584","DOIUrl":"https://doi.org/10.2514/6.2018-3584","url":null,"abstract":"","PeriodicalId":326346,"journal":{"name":"2018 Modeling and Simulation Technologies Conference","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"115199043","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: 0
Monte Carlo Simulation Based Design of a Robust Autopilot for Loitering Aerial Vehicles 基于蒙特卡罗仿真的飞行飞行器鲁棒自动驾驶仪设计
2018 Modeling and Simulation Technologies Conference Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3889
O. H. Altintas
{"title":"Monte Carlo Simulation Based Design of a Robust Autopilot for Loitering Aerial Vehicles","authors":"O. H. Altintas","doi":"10.2514/6.2018-3889","DOIUrl":"https://doi.org/10.2514/6.2018-3889","url":null,"abstract":"","PeriodicalId":326346,"journal":{"name":"2018 Modeling and Simulation Technologies Conference","volume":"6 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129620262","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: 0
A novel framework approach enabling Model-based Requirements Validation and Verification 一种新颖的框架方法，支持基于模型的需求确认和验证
2018 Modeling and Simulation Technologies Conference Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3892
Bastian Binder, M. Gottschall, T. Blochwitz
{"title":"A novel framework approach enabling Model-based Requirements Validation and Verification","authors":"Bastian Binder, M. Gottschall, T. Blochwitz","doi":"10.2514/6.2018-3892","DOIUrl":"https://doi.org/10.2514/6.2018-3892","url":null,"abstract":"","PeriodicalId":326346,"journal":{"name":"2018 Modeling and Simulation Technologies Conference","volume":"53 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126008629","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: 1
Verifying Implementation of the Dryden Turbulence Model and MIL-F-8785 Gust Gradient Dryden湍流模型和MIL-F-8785阵风梯度的验证实现
2018 Modeling and Simulation Technologies Conference Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3580
Michael M. Madden
{"title":"Verifying Implementation of the Dryden Turbulence Model and MIL-F-8785 Gust Gradient","authors":"Michael M. Madden","doi":"10.2514/6.2018-3580","DOIUrl":"https://doi.org/10.2514/6.2018-3580","url":null,"abstract":"Turbulence modeling in human-in-the-loop simulation is important to assessing aircraft handling qualities and pilot performance and to provide additional realism for pilot training. In the simulation community, the Dryden turbulence spectra is a popular choice for modeling the linear turbulent gusts because its rational form is efficiently reproduced by passing white noise through linear filters. The MIL-F-8785 gust gradients similarly use additional linear filters to model the gradient of the turbulent gust over the wing, and it represents the gust gradients as perturbations to the air-relative rotational rates. The Cockpit Motion Facility at NASA Langley Research Center (LaRC) models continuous random turbulence using the Dryden one-dimensional spectra and MIL-F-8785 gust gradient. The facility recently reviewed and updated its verification of these models as part of an initiative to improve motion cueing under turbulence. This exercise introduced improved methods for verifying the turbulence models and led to rediscovery of model assumptions that informed improvements to implementation.","PeriodicalId":326346,"journal":{"name":"2018 Modeling and Simulation Technologies Conference","volume":"51 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126500117","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: 1
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