Pub Date : 2009-12-04DOI: 10.1109/DASC.2009.5347480
Maxime Gariel, E. Feron
This paper presents a 3D conflict avoidance algorithm in the presence of uncertainty. The objective of the algorithm is to ensure the safety of the airspace in the event of a failure in the communication, navigation or surveillance systems. The algorithm minimizes the number of maneuvers required to maintain the safety of the airspace under degraded conditions. Uncertainties are modeled as an increase in the required separation distance between aircraft. A single maneuver for each aircraft is chosen to maintain safe separation. Maneuvers include heading change, speed change and flight level change. Maneuvers are simple to execute and guarantee a conflict-free configuration after execution. Their feasibility is constrained by weather avoidance, sector boundaries and aircraft performance. A Mixed Integer Program is used to determine the set of maneuvers to be executed.
{"title":"3D conflict avoidance under uncertainties","authors":"Maxime Gariel, E. Feron","doi":"10.1109/DASC.2009.5347480","DOIUrl":"https://doi.org/10.1109/DASC.2009.5347480","url":null,"abstract":"This paper presents a 3D conflict avoidance algorithm in the presence of uncertainty. The objective of the algorithm is to ensure the safety of the airspace in the event of a failure in the communication, navigation or surveillance systems. The algorithm minimizes the number of maneuvers required to maintain the safety of the airspace under degraded conditions. Uncertainties are modeled as an increase in the required separation distance between aircraft. A single maneuver for each aircraft is chosen to maintain safe separation. Maneuvers include heading change, speed change and flight level change. Maneuvers are simple to execute and guarantee a conflict-free configuration after execution. Their feasibility is constrained by weather avoidance, sector boundaries and aircraft performance. A Mixed Integer Program is used to determine the set of maneuvers to be executed.","PeriodicalId":313168,"journal":{"name":"2009 IEEE/AIAA 28th Digital Avionics Systems Conference","volume":"236 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2009-12-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"120880309","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}
Pub Date : 2009-12-04DOI: 10.1109/DASC.2009.5347482
T. Seliga, D. Hazen, L. Salcedo
The widespread placement of Runway Visual Range (RVR) visibility sensors over an airport domain provides an opportunity to expand their utility to other airport applications. These include determining visibility and inferring equivalent liquid water content snowfall rates anywhere on the airport surface. The interpolation of extinction coefficient measurements is demonstrated at Denver International Airport (DEN) and Portland International Airport (PDX). The snowfall rate determination is demonstrated at DEN, using calibration of visibility sensor extinction coefficient measurements based on an equivalent snowfall water content gauge located nearby one of the RVR visibility sensors. The snowfall rate data are shown to be useful for tracking equivalent liquid water snowfall amounts that can accumulate on an aircraft during taxiing from a deicing station to a takeoff position on a runway. This tracking of snowfall impinging on an aircraft along its designated surface route should help ensure safer deicing decision making. Furthermore, ongoing evaluation of aircraft tracks for takeoff on different runways can provide controllers with options on runway selection to enhance capacity. The time portrayal of interpolated images of visibility at DEN and PDX demonstrates how visibility can differ significantly over an airport surface and how this visibility can drift in time. Similar to the snowfall application, the interpolated visibility along surface routes to and from runways can help controllers improve estimates of times required for safe transit of aircraft during taxiing.
{"title":"Possible enhancements of airport operations based on runway visual range visibility measurements","authors":"T. Seliga, D. Hazen, L. Salcedo","doi":"10.1109/DASC.2009.5347482","DOIUrl":"https://doi.org/10.1109/DASC.2009.5347482","url":null,"abstract":"The widespread placement of Runway Visual Range (RVR) visibility sensors over an airport domain provides an opportunity to expand their utility to other airport applications. These include determining visibility and inferring equivalent liquid water content snowfall rates anywhere on the airport surface. The interpolation of extinction coefficient measurements is demonstrated at Denver International Airport (DEN) and Portland International Airport (PDX). The snowfall rate determination is demonstrated at DEN, using calibration of visibility sensor extinction coefficient measurements based on an equivalent snowfall water content gauge located nearby one of the RVR visibility sensors. The snowfall rate data are shown to be useful for tracking equivalent liquid water snowfall amounts that can accumulate on an aircraft during taxiing from a deicing station to a takeoff position on a runway. This tracking of snowfall impinging on an aircraft along its designated surface route should help ensure safer deicing decision making. Furthermore, ongoing evaluation of aircraft tracks for takeoff on different runways can provide controllers with options on runway selection to enhance capacity. The time portrayal of interpolated images of visibility at DEN and PDX demonstrates how visibility can differ significantly over an airport surface and how this visibility can drift in time. Similar to the snowfall application, the interpolated visibility along surface routes to and from runways can help controllers improve estimates of times required for safe transit of aircraft during taxiing.","PeriodicalId":313168,"journal":{"name":"2009 IEEE/AIAA 28th Digital Avionics Systems Conference","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2009-12-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130999905","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}
Pub Date : 2009-12-04DOI: 10.1109/DASC.2009.5347556
T. Prevot, San José
This paper describes technologies for mid-term and far-term air traffic control operations in the Next Generation Air Transportation System (NextGen). The technologies were developed and evaluated with human-in-the-loop simulations in the Airspace Operations Laboratory (AOL) at the NASA Ames Research Center. The simulations were funded by several research focus areas within NASA's Airspace Systems program and some were co-funded by the FAA's Air Traffic Organization for Planning, Research and Technology. Results indicate that advanced trajectory-based air traffic control automation at the controller workstation integrated with data com and moderate flight deck upgrades shows great promise to increase airspace capacity significantly in the mid-term and far-term.
{"title":"NextGen technologies for mid-term and far-term air traffic control operations","authors":"T. Prevot, San José","doi":"10.1109/DASC.2009.5347556","DOIUrl":"https://doi.org/10.1109/DASC.2009.5347556","url":null,"abstract":"This paper describes technologies for mid-term and far-term air traffic control operations in the Next Generation Air Transportation System (NextGen). The technologies were developed and evaluated with human-in-the-loop simulations in the Airspace Operations Laboratory (AOL) at the NASA Ames Research Center. The simulations were funded by several research focus areas within NASA's Airspace Systems program and some were co-funded by the FAA's Air Traffic Organization for Planning, Research and Technology. Results indicate that advanced trajectory-based air traffic control automation at the controller workstation integrated with data com and moderate flight deck upgrades shows great promise to increase airspace capacity significantly in the mid-term and far-term.","PeriodicalId":313168,"journal":{"name":"2009 IEEE/AIAA 28th Digital Avionics Systems Conference","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2009-12-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"131159413","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}
Pub Date : 2009-12-04DOI: 10.1109/DASC.2009.5347467
Julian Sanchez, E. Zakrzewski
A decision support aid to assist controllers in merging Area Navigation (RNAV) flows was evaluated by the MITRE Corporation's Center for Advanced Aviation System Development (CAASD). The goal of this effort was to gather objective performance data to quantify the benefits of an automation prototype on the demands of the Air Traffic Control (ATC) task. A dual-task methodology was used to assess the spare cognitive/perceptual resources of an experienced controller when managing traffic with and without the automation. Two implementations of the automation were evaluated, one where the controller communicated with the flight crew via voice and another via datalink. The results suggest that a dual-task methodology can help quantify the benefits of ATC automation in terms of assessing controller cognitive/perceptual resources.
{"title":"The impact of ATC automation on a controller's visual attention","authors":"Julian Sanchez, E. Zakrzewski","doi":"10.1109/DASC.2009.5347467","DOIUrl":"https://doi.org/10.1109/DASC.2009.5347467","url":null,"abstract":"A decision support aid to assist controllers in merging Area Navigation (RNAV) flows was evaluated by the MITRE Corporation's Center for Advanced Aviation System Development (CAASD). The goal of this effort was to gather objective performance data to quantify the benefits of an automation prototype on the demands of the Air Traffic Control (ATC) task. A dual-task methodology was used to assess the spare cognitive/perceptual resources of an experienced controller when managing traffic with and without the automation. Two implementations of the automation were evaluated, one where the controller communicated with the flight crew via voice and another via datalink. The results suggest that a dual-task methodology can help quantify the benefits of ATC automation in terms of assessing controller cognitive/perceptual resources.","PeriodicalId":313168,"journal":{"name":"2009 IEEE/AIAA 28th Digital Avionics Systems Conference","volume":"62 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2009-12-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126641825","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}
Pub Date : 2009-12-04DOI: 10.1109/DASC.2009.5347443
S. Ray, G. Karsai, K. Mcneill
In this paper we describe our experience applying the Producible Adaptive Model-based Software (PAMS) technology to the development of safety critical flight control software. PAMS is based on the state of the art Model Integrated Computing (MIC) environment from Vanderbilt University and represents a highly evolvable model-based software development methodology and tool suite that is revolutionary in its ability to address software adaptation. In particular, PAMS is an adaptation framework that introduces support for model transformations, co-evolution of models and modeling tools, and self-adaptation of systems. Analogous to delayed binding in compiler technology, PAMS enables binding software updates statically at design-time, on a configuration basis at load-time, and dynamically at run-time. The focus of this paper will be the application of PAMS to designtime evolution.
{"title":"Model-based adaptation of flight-critical systems","authors":"S. Ray, G. Karsai, K. Mcneill","doi":"10.1109/DASC.2009.5347443","DOIUrl":"https://doi.org/10.1109/DASC.2009.5347443","url":null,"abstract":"In this paper we describe our experience applying the Producible Adaptive Model-based Software (PAMS) technology to the development of safety critical flight control software. PAMS is based on the state of the art Model Integrated Computing (MIC) environment from Vanderbilt University and represents a highly evolvable model-based software development methodology and tool suite that is revolutionary in its ability to address software adaptation. In particular, PAMS is an adaptation framework that introduces support for model transformations, co-evolution of models and modeling tools, and self-adaptation of systems. Analogous to delayed binding in compiler technology, PAMS enables binding software updates statically at design-time, on a configuration basis at load-time, and dynamically at run-time. The focus of this paper will be the application of PAMS to designtime evolution.","PeriodicalId":313168,"journal":{"name":"2009 IEEE/AIAA 28th Digital Avionics Systems Conference","volume":"91 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2009-12-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126655858","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}
Pub Date : 2009-12-04DOI: 10.1109/DASC.2009.5347439
J. Simon, M. Braasch
Unmanned Aerial Vehicles (UAVs) are becoming more prevalent in military applications and through the success of these applications, many commercial usages have been derived. However, due to the recent development of UAVs, the Federal Aviation Administration (FAA) has not yet been able to develop performance requirements for the Detect, Sense, and Avoid (DSA) system of UAVs. For this reason, this study serves to explore the current capabilities of human general aviation (GA) pilots with regards to their see-and-avoid abilities. The midair collision rate over the past ten years and the average traffic around an average airport are also explored. With the analyzed data, a model is developed in order to extract the grounds for performance requirement for DSA systems. The determined DSA performance number can be used to further aid in the development of overall performance requirements for DSA systems.
{"title":"Deriving sensible requirements for UAV sense-and-avoid systems","authors":"J. Simon, M. Braasch","doi":"10.1109/DASC.2009.5347439","DOIUrl":"https://doi.org/10.1109/DASC.2009.5347439","url":null,"abstract":"Unmanned Aerial Vehicles (UAVs) are becoming more prevalent in military applications and through the success of these applications, many commercial usages have been derived. However, due to the recent development of UAVs, the Federal Aviation Administration (FAA) has not yet been able to develop performance requirements for the Detect, Sense, and Avoid (DSA) system of UAVs. For this reason, this study serves to explore the current capabilities of human general aviation (GA) pilots with regards to their see-and-avoid abilities. The midair collision rate over the past ten years and the average traffic around an average airport are also explored. With the analyzed data, a model is developed in order to extract the grounds for performance requirement for DSA systems. The determined DSA performance number can be used to further aid in the development of overall performance requirements for DSA systems.","PeriodicalId":313168,"journal":{"name":"2009 IEEE/AIAA 28th Digital Avionics Systems Conference","volume":"283 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2009-12-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122956090","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}
Pub Date : 2009-12-04DOI: 10.1109/DASC.2009.5347430
J. M. Canino, L. Gómez, J. García, J. Besada, J. Casar
Current and future air traffic is requiring new procedures and systems to achieve a greater automation of air-traffic operations. Particular difficulty presents the automation of arrival air-traffic operations in terminal areas due to aircraft speeds and environment variability into a delimited airspace where multiple aircraft converge. Several projects have proposed guidelines to implement new operational concepts as well as airborne and ground systems to carry out corresponding procedures. Developing procedures and systems are closely related. Therefore, usually it requires to analyze and to design them in a combined manner. In this paper we present an agent-oriented analysis and modeling of airborne systems capabilities to perform automated arrival and approach procedures based on user preference trajectories. A detailed architecture model of airborne capabilities is achieved through a methodological analysis of an arrival traffic scenario within the trajectory based operations paradigm.
{"title":"An agent oriented analysis and modeling of airborne capabilities for trajectory based operations","authors":"J. M. Canino, L. Gómez, J. García, J. Besada, J. Casar","doi":"10.1109/DASC.2009.5347430","DOIUrl":"https://doi.org/10.1109/DASC.2009.5347430","url":null,"abstract":"Current and future air traffic is requiring new procedures and systems to achieve a greater automation of air-traffic operations. Particular difficulty presents the automation of arrival air-traffic operations in terminal areas due to aircraft speeds and environment variability into a delimited airspace where multiple aircraft converge. Several projects have proposed guidelines to implement new operational concepts as well as airborne and ground systems to carry out corresponding procedures. Developing procedures and systems are closely related. Therefore, usually it requires to analyze and to design them in a combined manner. In this paper we present an agent-oriented analysis and modeling of airborne systems capabilities to perform automated arrival and approach procedures based on user preference trajectories. A detailed architecture model of airborne capabilities is achieved through a methodological analysis of an arrival traffic scenario within the trajectory based operations paradigm.","PeriodicalId":313168,"journal":{"name":"2009 IEEE/AIAA 28th Digital Avionics Systems Conference","volume":"15 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2009-12-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114777136","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}
Pub Date : 2009-12-04DOI: 10.1109/DASC.2009.5347483
A. Senoguchi, T. Koga
In order to prepare for future deployment of SSR (Secondary Surveillance Radar) Mode S with DAPs (Downlink Aircraft Parameters) function in Japan, ENRI (Electronic Navigation Research Institute) has started research and development of new SSR Mode S. DAPs function enables ground station to obtain aircraft information such as selected altitude, rollangle, magnetic heading and so on. When DAPs function is employed as a means of ATC (Air Traffic Control), reliability of DAPs data is critically important. The purpose of this paper is to compare DAPs data with original FMS (Flight Management System) source data to validate radar system function and to test the reliability of DAPs data. This time, we picked up B737–800 and B747-400 and selected aircraft parameters in GICB (Ground Initiated Comm-B) 40, 50 and 60 as an analysis target of DAPs data. These are known as Mode S EHS (Enhanced Surveillance) which becomes mandatory in the part of Europe. In this paper, we first describe our experimental Mode S system with DAPs function. Then, DAPs data have been compared with the data stored in aircraft flight recorder. As a result, we presented that the values of DAPs agreed with those of airborne stored data except in a few parameters.
{"title":"Analysis of downlink aircraft parameters monitored by SSR mode S in ENRI","authors":"A. Senoguchi, T. Koga","doi":"10.1109/DASC.2009.5347483","DOIUrl":"https://doi.org/10.1109/DASC.2009.5347483","url":null,"abstract":"In order to prepare for future deployment of SSR (Secondary Surveillance Radar) Mode S with DAPs (Downlink Aircraft Parameters) function in Japan, ENRI (Electronic Navigation Research Institute) has started research and development of new SSR Mode S. DAPs function enables ground station to obtain aircraft information such as selected altitude, rollangle, magnetic heading and so on. When DAPs function is employed as a means of ATC (Air Traffic Control), reliability of DAPs data is critically important. The purpose of this paper is to compare DAPs data with original FMS (Flight Management System) source data to validate radar system function and to test the reliability of DAPs data. This time, we picked up B737–800 and B747-400 and selected aircraft parameters in GICB (Ground Initiated Comm-B) 40, 50 and 60 as an analysis target of DAPs data. These are known as Mode S EHS (Enhanced Surveillance) which becomes mandatory in the part of Europe. In this paper, we first describe our experimental Mode S system with DAPs function. Then, DAPs data have been compared with the data stored in aircraft flight recorder. As a result, we presented that the values of DAPs agreed with those of airborne stored data except in a few parameters.","PeriodicalId":313168,"journal":{"name":"2009 IEEE/AIAA 28th Digital Avionics Systems Conference","volume":"52 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2009-12-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"124338699","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}
Pub Date : 2009-12-04DOI: 10.1109/DASC.2009.5347528
Leihong Li, J. Clarke, H. C. Chien, Terran Melconian
Local meteorological conditions such as wind direction, cloud ceiling heights, and visibility directly influence the safety and efficiency of an airport. The safety and efficiency, generally contradictory, are associated with the selection of a particular runway configuration that is a part of job of airport tower controllers. When the wind speed and directions exceed the maximum allowable limit defined by the FAA operational procedures, controllers must change runway configurations. During this configuration change, the status of all arriving and departing aircrafts are turned into airborne or ground holding, respectively, until the new flight paths and the new taxi paths are clarified. This situation greatly influences the airport operational efficiency with its associated cost of delays, fuel burn and emissions. Despite its prominence, only a few studies that discuss the timing of decision-making for the configuration change can be found. In this study, an innovative decision-making approach is proposed for runway configuration planning under stochastic wind conditions. The goal of the decision-making approach is to maximize the airport throughput and minimize the airborne delay in terminal area, given a sequence of wind forecast data. The optimization techniques of dynamic programming and backwards induction are used to solve the probabilistic optimality equation. Based on the simulation results of JFK test case, the proposed approach is shown to reduce the average delay time and improve the throughput of runway systems without violating operational procedures.
{"title":"A probabilistic decision-making model for runway configuration planning under stochastic wind conditions","authors":"Leihong Li, J. Clarke, H. C. Chien, Terran Melconian","doi":"10.1109/DASC.2009.5347528","DOIUrl":"https://doi.org/10.1109/DASC.2009.5347528","url":null,"abstract":"Local meteorological conditions such as wind direction, cloud ceiling heights, and visibility directly influence the safety and efficiency of an airport. The safety and efficiency, generally contradictory, are associated with the selection of a particular runway configuration that is a part of job of airport tower controllers. When the wind speed and directions exceed the maximum allowable limit defined by the FAA operational procedures, controllers must change runway configurations. During this configuration change, the status of all arriving and departing aircrafts are turned into airborne or ground holding, respectively, until the new flight paths and the new taxi paths are clarified. This situation greatly influences the airport operational efficiency with its associated cost of delays, fuel burn and emissions. Despite its prominence, only a few studies that discuss the timing of decision-making for the configuration change can be found. In this study, an innovative decision-making approach is proposed for runway configuration planning under stochastic wind conditions. The goal of the decision-making approach is to maximize the airport throughput and minimize the airborne delay in terminal area, given a sequence of wind forecast data. The optimization techniques of dynamic programming and backwards induction are used to solve the probabilistic optimality equation. Based on the simulation results of JFK test case, the proposed approach is shown to reduce the average delay time and improve the throughput of runway systems without violating operational procedures.","PeriodicalId":313168,"journal":{"name":"2009 IEEE/AIAA 28th Digital Avionics Systems Conference","volume":"388 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2009-12-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123198549","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}
Pub Date : 2009-12-04DOI: 10.1109/DASC.2009.5347561
M. Jakovljević
Not Available for Publication
无法出版
{"title":"Distributed IMA software platforms using synchronized ARINC653 operating systems","authors":"M. Jakovljević","doi":"10.1109/DASC.2009.5347561","DOIUrl":"https://doi.org/10.1109/DASC.2009.5347561","url":null,"abstract":"Not Available for Publication","PeriodicalId":313168,"journal":{"name":"2009 IEEE/AIAA 28th Digital Avionics Systems Conference","volume":"31 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2009-12-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123205508","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}
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