Pub Date : 2020-09-01DOI: 10.1109/ICNS50378.2020.9222911
Tao Li
It has been shown that flights can potentially achieve a significant amount of fuel burn reduction by flying the wind-optimal trajectories. This study estimates the benefits of flying the wind-optimal trajectory in the Pacific airspace using a simulation approach. Using the forecast of the 2020 traffic in the airspace, we found that airlines can save about 14,600 flight hours and 14 million gallons of fuel by using the wind-optimal trajectories inside the airspace. Depending on the Jet-A fuel price, the monetary value of the fuel savings ranges from 13 million dollars to 30 million dollars. There will also be a significant reduction in the workload of air traffic controllers and pilots.
{"title":"Evaluating the Benefits of Flying Wind-Optimal Trajectory Inside the Pacific Airspace","authors":"Tao Li","doi":"10.1109/ICNS50378.2020.9222911","DOIUrl":"https://doi.org/10.1109/ICNS50378.2020.9222911","url":null,"abstract":"It has been shown that flights can potentially achieve a significant amount of fuel burn reduction by flying the wind-optimal trajectories. This study estimates the benefits of flying the wind-optimal trajectory in the Pacific airspace using a simulation approach. Using the forecast of the 2020 traffic in the airspace, we found that airlines can save about 14,600 flight hours and 14 million gallons of fuel by using the wind-optimal trajectories inside the airspace. Depending on the Jet-A fuel price, the monetary value of the fuel savings ranges from 13 million dollars to 30 million dollars. There will also be a significant reduction in the workload of air traffic controllers and pilots.","PeriodicalId":424869,"journal":{"name":"2020 Integrated Communications Navigation and Surveillance Conference (ICNS)","volume":"15 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2020-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"125686353","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 : 2020-09-01DOI: 10.1109/ICNS50378.2020.9222891
Tao Li
The hemispherical rules require that eastbound flights should use odd thousands flight levels (FLs) and westbound flights should use even thousands FLs. Though these rules improve safety, they could also negatively impact flight efficiency by, for example, reducing the available FLs that can be used to improve efficiency. With improved surveillance and communication capabilities in oceanic airspace, it is possible to use the FLs that do not comply with the hemispherical rules (non-complying FLs). The paper investigates whether doing so in the Pacific airspace could bring benefits to airlines and air traffic controllers. Our analysis showed mixed results. We found that fuel savings would increase as more flights accept non-complying FLs. If all flights accept non-complying FLs, the annual total fuel savings could reach 12.2 million gallons within the Oakland and Anchorage Flight Information Region (FIR). Depending on the price of Jet-A fuel, the monetary value of these fuel savings ranges from 11.25 to 25.66 million dollars. However, we also found that the annual total travel time inside the two FIRs would increase by about 2,070 flight hours. In addition, the workload of air traffic controllers and pilots may also increase as more flights accept non-complying FLs.
{"title":"Evaluating the Benefits of Accepting Cruising Flight Levels That Are Not in Compliance with the Hemispherical Rules in the Pacific Airspace","authors":"Tao Li","doi":"10.1109/ICNS50378.2020.9222891","DOIUrl":"https://doi.org/10.1109/ICNS50378.2020.9222891","url":null,"abstract":"The hemispherical rules require that eastbound flights should use odd thousands flight levels (FLs) and westbound flights should use even thousands FLs. Though these rules improve safety, they could also negatively impact flight efficiency by, for example, reducing the available FLs that can be used to improve efficiency. With improved surveillance and communication capabilities in oceanic airspace, it is possible to use the FLs that do not comply with the hemispherical rules (non-complying FLs). The paper investigates whether doing so in the Pacific airspace could bring benefits to airlines and air traffic controllers. Our analysis showed mixed results. We found that fuel savings would increase as more flights accept non-complying FLs. If all flights accept non-complying FLs, the annual total fuel savings could reach 12.2 million gallons within the Oakland and Anchorage Flight Information Region (FIR). Depending on the price of Jet-A fuel, the monetary value of these fuel savings ranges from 11.25 to 25.66 million dollars. However, we also found that the annual total travel time inside the two FIRs would increase by about 2,070 flight hours. In addition, the workload of air traffic controllers and pilots may also increase as more flights accept non-complying FLs.","PeriodicalId":424869,"journal":{"name":"2020 Integrated Communications Navigation and Surveillance Conference (ICNS)","volume":"45 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2020-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133781032","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 : 2020-09-01DOI: 10.1109/ICNS50378.2020.9223004
Yutong Chen, Lei Yang, Haoran Zhang, Zheng Zhao, Minghua Hu
Aiming at achieving the autonomous Air Traffic Management (ATM) in the Trajectory-Based Operation (TBO) context, a two-stage real-time autonomous four-dimensional trajectory conflict detection and resolution method in restricted Free Route Airspace (FRA) supporting the synchronized air-ground situational awareness was proposed. Cellular concept was used for airspace discretization to balance the accuracy and computation cost. At stage one, the desired trajectory for each upcoming flight is generated by searching a path in a network constructed based on the entry and exit point, as well as boundary points of each restricted area inside the airspace. At stage two, in order to avoid conflict during travelling, the Space-Time Prism model, which is capable of visualizing the conflict situation for both controllers and pilots, is introduced to generate the feasible conflict-free trajectories while keeping the Controlled Time of Arrival (CTA) in mind. A case study based on a typical en route sector in Western China was carried out to test the effectiveness of the proposed method. In the end, sensitivity of cell size was investigated in terms of computational cost and operational efficiency. Results showed that the proposed autonomous trajectory planning would be a promising solution for future autonomous ATM system.
{"title":"Real-Time Autonomous Trajectory Conflict Detection and Resolution in Restricted Airspace","authors":"Yutong Chen, Lei Yang, Haoran Zhang, Zheng Zhao, Minghua Hu","doi":"10.1109/ICNS50378.2020.9223004","DOIUrl":"https://doi.org/10.1109/ICNS50378.2020.9223004","url":null,"abstract":"Aiming at achieving the autonomous Air Traffic Management (ATM) in the Trajectory-Based Operation (TBO) context, a two-stage real-time autonomous four-dimensional trajectory conflict detection and resolution method in restricted Free Route Airspace (FRA) supporting the synchronized air-ground situational awareness was proposed. Cellular concept was used for airspace discretization to balance the accuracy and computation cost. At stage one, the desired trajectory for each upcoming flight is generated by searching a path in a network constructed based on the entry and exit point, as well as boundary points of each restricted area inside the airspace. At stage two, in order to avoid conflict during travelling, the Space-Time Prism model, which is capable of visualizing the conflict situation for both controllers and pilots, is introduced to generate the feasible conflict-free trajectories while keeping the Controlled Time of Arrival (CTA) in mind. A case study based on a typical en route sector in Western China was carried out to test the effectiveness of the proposed method. In the end, sensitivity of cell size was investigated in terms of computational cost and operational efficiency. Results showed that the proposed autonomous trajectory planning would be a promising solution for future autonomous ATM system.","PeriodicalId":424869,"journal":{"name":"2020 Integrated Communications Navigation and Surveillance Conference (ICNS)","volume":"61 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2020-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133479070","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 : 2020-09-01DOI: 10.1109/ICNS50378.2020.9222886
E. Theunissen, W. Zijlstra
Minimum Detect and avoid Well Clear (DWC) guidance provides the pilot with information on the directions in which DWC is predicted to be lost and how soon. Different guidance algorithms are analyzed for their ability to provide guidance after DWC is lost. Command and status-based concepts for guidance to regain-DWC in case the loss was not prevented are compared from a conceptual, regulatory and performance perspective. The guidance decisions and associated performance are analyzed using TCPA-DCPA traces and guidance band time-histories. Based on the results, recommendations are provided.
{"title":"Comparing Regain Well Clear Guidance","authors":"E. Theunissen, W. Zijlstra","doi":"10.1109/ICNS50378.2020.9222886","DOIUrl":"https://doi.org/10.1109/ICNS50378.2020.9222886","url":null,"abstract":"Minimum Detect and avoid Well Clear (DWC) guidance provides the pilot with information on the directions in which DWC is predicted to be lost and how soon. Different guidance algorithms are analyzed for their ability to provide guidance after DWC is lost. Command and status-based concepts for guidance to regain-DWC in case the loss was not prevented are compared from a conceptual, regulatory and performance perspective. The guidance decisions and associated performance are analyzed using TCPA-DCPA traces and guidance band time-histories. Based on the results, recommendations are provided.","PeriodicalId":424869,"journal":{"name":"2020 Integrated Communications Navigation and Surveillance Conference (ICNS)","volume":"28 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2020-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114942714","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 : 2020-09-01DOI: 10.1109/ICNS50378.2020.9222863
Jungmin Seo, A. Izadi, A. Trani
The Federal Aviation Administration (FAA) Weather Technology in the Cockpit (WTIC) program has sponsored an operational demonstration to provide satellite-based meteorological information to commercial flights in remote and oceanic regions. This effort is called the Remote Oceanic Meteorology Information Operational (ROMIO) demonstration. For this effort, the National Center of Atmospheric Research (NCAR) developed two weather products: 1) Cloud Top Height (CTH), and 2) Convection Diagnosis Oceanic (CDO). The CTH product displays cloud top contours at flight altitudes of FL320, FL340, FL360, FL380, and FL400. The CDO product displays hazards associated with the storm updraft, lightning, and overshooting tops in four intensity levels (medium, high, severe, and extreme).In this paper, we study the potential benefits of the ROMIO demonstration through survey analysis to measure pilots’ acceptance and the ROMIO-aided behavior during en-route convective weather avoidance. We created a post-flight pilot survey to have a qualitative measure of the benefits of using the ROMIO application and to assess users' acceptance of the new airborne information technology. The questions in the questionnaire were mainly categorized into five groups: 1) decision-making, 2) workload, 3) situational awareness, 4) efficiency, and 5) quality of information. We applied Wilcoxon’s rank-sum test to analyze Likert scale responses. The study includes 105 pilot survey responses. The results of this study improve our understanding of the potential benefits of new airborne weather information technology from the pilots’ perspective and allow us to identify potential areas for further improvement of the ROMIO demonstration.
{"title":"Operational Benefits of Remote Oceanic Meteorology Information Operational (Romio) Demonstration: A Survey-Based Analysis","authors":"Jungmin Seo, A. Izadi, A. Trani","doi":"10.1109/ICNS50378.2020.9222863","DOIUrl":"https://doi.org/10.1109/ICNS50378.2020.9222863","url":null,"abstract":"The Federal Aviation Administration (FAA) Weather Technology in the Cockpit (WTIC) program has sponsored an operational demonstration to provide satellite-based meteorological information to commercial flights in remote and oceanic regions. This effort is called the Remote Oceanic Meteorology Information Operational (ROMIO) demonstration. For this effort, the National Center of Atmospheric Research (NCAR) developed two weather products: 1) Cloud Top Height (CTH), and 2) Convection Diagnosis Oceanic (CDO). The CTH product displays cloud top contours at flight altitudes of FL320, FL340, FL360, FL380, and FL400. The CDO product displays hazards associated with the storm updraft, lightning, and overshooting tops in four intensity levels (medium, high, severe, and extreme).In this paper, we study the potential benefits of the ROMIO demonstration through survey analysis to measure pilots’ acceptance and the ROMIO-aided behavior during en-route convective weather avoidance. We created a post-flight pilot survey to have a qualitative measure of the benefits of using the ROMIO application and to assess users' acceptance of the new airborne information technology. The questions in the questionnaire were mainly categorized into five groups: 1) decision-making, 2) workload, 3) situational awareness, 4) efficiency, and 5) quality of information. We applied Wilcoxon’s rank-sum test to analyze Likert scale responses. The study includes 105 pilot survey responses. The results of this study improve our understanding of the potential benefits of new airborne weather information technology from the pilots’ perspective and allow us to identify potential areas for further improvement of the ROMIO demonstration.","PeriodicalId":424869,"journal":{"name":"2020 Integrated Communications Navigation and Surveillance Conference (ICNS)","volume":"25 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2020-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"121149639","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 : 2020-09-01DOI: 10.1109/ICNS50378.2020.9222908
James Keller, B. Deng, David Gore
Effective surveillance of non-cooperative targets is necessary to enable Beyond Visual Line of Sight (BVLOS) flights for small Unmanned Aerial Systems (sUAS). We examine several approaches to develop effective surveillance for non-cooperative targets within the typical sUAS operations arena (low altitude, Class G airspace), to determine suitability for situational awareness and Detect and Avoid (DAA). This ongoing research includes analysis of sensor performance and determination of applicability to the sUAS mission. Effective surveillance for cooperative manned targets is easier to achieve using ADS-B; however, there is no current solution for cooperatively tracking sUAS, which have been restricted from using ADS-B. Until Remote ID is available, surveillance of UAS must be performed through non-cooperative means. While the safety focus is on situational awareness and DAA for manned aircraft, we also consider UAS non-cooperative surveillance as part of the study. We provide initial conclusions and outline a path for additional research.
{"title":"Effective Non-Cooperative Surveillance for UAS Situational Awareness","authors":"James Keller, B. Deng, David Gore","doi":"10.1109/ICNS50378.2020.9222908","DOIUrl":"https://doi.org/10.1109/ICNS50378.2020.9222908","url":null,"abstract":"Effective surveillance of non-cooperative targets is necessary to enable Beyond Visual Line of Sight (BVLOS) flights for small Unmanned Aerial Systems (sUAS). We examine several approaches to develop effective surveillance for non-cooperative targets within the typical sUAS operations arena (low altitude, Class G airspace), to determine suitability for situational awareness and Detect and Avoid (DAA). This ongoing research includes analysis of sensor performance and determination of applicability to the sUAS mission. Effective surveillance for cooperative manned targets is easier to achieve using ADS-B; however, there is no current solution for cooperatively tracking sUAS, which have been restricted from using ADS-B. Until Remote ID is available, surveillance of UAS must be performed through non-cooperative means. While the safety focus is on situational awareness and DAA for manned aircraft, we also consider UAS non-cooperative surveillance as part of the study. We provide initial conclusions and outline a path for additional research.","PeriodicalId":424869,"journal":{"name":"2020 Integrated Communications Navigation and Surveillance Conference (ICNS)","volume":"8 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2020-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"131950068","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 : 2020-09-01DOI: 10.1109/ICNS50378.2020.9222944
A. Young, David Luong, B. Balaji, S. Rajan
The detection and parametric estimation of low-SNR radar signals, particularly linear frequency modulated (LFM) radar signals, is a problem of considerable interest. In prior work, this problem has been investigated using various signal processing techniques, such as maximum likelihood estimation, fractional Fourier transform and Wigner-Ville-based methods, to analyze the signal parameters of a complex linear frequency modulated signal. Other work has focused on applying deep learning to automatically recognize various radar waveform types and their features, such as linear frequency modulation (LFM), Barker code and rectangular waveforms. In this paper, we investigate this problem from a machine learning perspective for multiple LFM radar signals given a priori information. We explore the use of naive Bayes, support vector machine and neural network classifiers to identify the LFM chirp rate, out of a set of known chirp rates, from a specific radar emitter under varying SNR conditions. Simulation results demonstrate the viability of this technique to identify the radar LFM mode in very low signal-to-noise ratio conditions down to -20 dB where using existing approaches (e.g., Wigner-Ville) fail.
{"title":"Machine Learning Approach to Chirp Rate Estimation of Linear Frequency Modulated Radars","authors":"A. Young, David Luong, B. Balaji, S. Rajan","doi":"10.1109/ICNS50378.2020.9222944","DOIUrl":"https://doi.org/10.1109/ICNS50378.2020.9222944","url":null,"abstract":"The detection and parametric estimation of low-SNR radar signals, particularly linear frequency modulated (LFM) radar signals, is a problem of considerable interest. In prior work, this problem has been investigated using various signal processing techniques, such as maximum likelihood estimation, fractional Fourier transform and Wigner-Ville-based methods, to analyze the signal parameters of a complex linear frequency modulated signal. Other work has focused on applying deep learning to automatically recognize various radar waveform types and their features, such as linear frequency modulation (LFM), Barker code and rectangular waveforms. In this paper, we investigate this problem from a machine learning perspective for multiple LFM radar signals given a priori information. We explore the use of naive Bayes, support vector machine and neural network classifiers to identify the LFM chirp rate, out of a set of known chirp rates, from a specific radar emitter under varying SNR conditions. Simulation results demonstrate the viability of this technique to identify the radar LFM mode in very low signal-to-noise ratio conditions down to -20 dB where using existing approaches (e.g., Wigner-Ville) fail.","PeriodicalId":424869,"journal":{"name":"2020 Integrated Communications Navigation and Surveillance Conference (ICNS)","volume":"72 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2020-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"134030182","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 : 2020-09-01DOI: 10.1109/ICNS50378.2020.9222974
Hossam O. Ahmed
The importance of the Unmanned Aircraft Systems (UAS) has been increased significantly nowadays due to the increasing demands on affording novel urban transportation system solutions that could leverage the transportation utilization ratio specially in congested urban cities. However, the viability of deploying Urban Air Mobility (UAM) solutions in our daily life depends on many critical safety factors. One of the most pivotal key players in the UAM safety aspect is their capability for accurately landing on narrow and unplanned urban lading spots. Subsequently, processing the elevation sensory data by depending on a single array-based sensor unit has many drawbacks in case of sudden electronically failure or spontaneous obstacle shadowing effects. In this paper, we proposed a multicore systolic real-time processing unit that is capable to increase the automation requirement levels for future UAMs through adopting parallel and complex sensory fusion computer architectures for increasing the accuracy of UAM during the landing process. The novel Fuzzy Logic System (FLS) processing unit is interactively dealing with Multiple Sensor Nodes (MSN) that are both frequency spectrum and spatially separated on the bottom side of an UAM. The proposed idea is surpassing the conventional single sensor-array based-solutions for UAM landing process in terms of improving the accuracy and safety concerns. The proposed systolic FLS architecture in this paper has been designed and tested using MATLAB and VHDL to be interfaced with five Lidar Sensors and five ultrasonic sensors using the Intel Altera OpenVINO FPGA board. The proposed systolic FLS processing unit achieved a processing computational speed of about 25.3 Giga Operations per Seconds (GOPS) and only 178.12 mW as core dynamic thermal power dissipation.
由于对提供新颖的城市交通系统解决方案的需求不断增加，特别是在拥挤的城市中，可以利用交通利用率，无人机系统(UAS)的重要性已经显著增加。然而，在我们的日常生活中部署城市空中交通(UAM)解决方案的可行性取决于许多关键的安全因素。UAM安全方面最关键的关键因素之一是它们在狭窄和计划外的城市提货点上准确着陆的能力。因此，在突发电子故障或自发障碍物阴影效应的情况下，依靠单个阵列传感器单元处理高程传感器数据存在许多缺点。在本文中，我们提出了一种多核收缩实时处理单元，该单元能够通过采用并行和复杂的感觉融合计算机架构来提高未来UAM的自动化要求水平，以提高UAM在着陆过程中的精度。新型模糊逻辑系统(FLS)处理单元交互式地处理位于UAM底部的多个传感器节点(MSN)，这些节点在频谱和空间上都是分离的。在提高精度和安全性方面，所提出的想法超越了传统的基于单传感器阵列的UAM着陆过程解决方案。利用MATLAB和VHDL对本文提出的收缩FLS架构进行了设计和测试，并利用Intel Altera OpenVINO FPGA板与五个激光雷达传感器和五个超声波传感器进行了接口。所提出的收缩FLS处理单元的处理计算速度约为25.3 Giga Operations per Seconds (GOPS)，核心动态热功耗仅为178.12 mW。
{"title":"25.3 GOPS Autonomous Landing Guidance Assistant System Using Systolic Fuzzy Logic System for Urban Air Mobility (UAM) Vehicles Using FPGA","authors":"Hossam O. Ahmed","doi":"10.1109/ICNS50378.2020.9222974","DOIUrl":"https://doi.org/10.1109/ICNS50378.2020.9222974","url":null,"abstract":"The importance of the Unmanned Aircraft Systems (UAS) has been increased significantly nowadays due to the increasing demands on affording novel urban transportation system solutions that could leverage the transportation utilization ratio specially in congested urban cities. However, the viability of deploying Urban Air Mobility (UAM) solutions in our daily life depends on many critical safety factors. One of the most pivotal key players in the UAM safety aspect is their capability for accurately landing on narrow and unplanned urban lading spots. Subsequently, processing the elevation sensory data by depending on a single array-based sensor unit has many drawbacks in case of sudden electronically failure or spontaneous obstacle shadowing effects. In this paper, we proposed a multicore systolic real-time processing unit that is capable to increase the automation requirement levels for future UAMs through adopting parallel and complex sensory fusion computer architectures for increasing the accuracy of UAM during the landing process. The novel Fuzzy Logic System (FLS) processing unit is interactively dealing with Multiple Sensor Nodes (MSN) that are both frequency spectrum and spatially separated on the bottom side of an UAM. The proposed idea is surpassing the conventional single sensor-array based-solutions for UAM landing process in terms of improving the accuracy and safety concerns. The proposed systolic FLS architecture in this paper has been designed and tested using MATLAB and VHDL to be interfaced with five Lidar Sensors and five ultrasonic sensors using the Intel Altera OpenVINO FPGA board. The proposed systolic FLS processing unit achieved a processing computational speed of about 25.3 Giga Operations per Seconds (GOPS) and only 178.12 mW as core dynamic thermal power dissipation.","PeriodicalId":424869,"journal":{"name":"2020 Integrated Communications Navigation and Surveillance Conference (ICNS)","volume":"2 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2020-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122242541","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 : 2020-09-01DOI: 10.1109/ICNS50378.2020.9222889
Z. Chaudhry, K. Fox
Air Traffic Management (ATM) is under great pressure and facing major challenges in the coming years. The industry is driven by safety, capacity, cost of service, efficiency and the environment. "Continuous traffic growth, structural airspace and airport capacity issues, and extreme weather events call for new approaches to reshape today’s operations and business models" [1]. If the aviation industry is to handle the levels of traffic predicted, as well as to cope with new flight modalities on the horizon, including Unmanned Aerial Systems (UAS) and space, "It will be essential to take a step forward in the capabilities of our systems to cope with the flood of data and to make intelligent decisions" [2].
{"title":"Artificial Intelligence Applicability to Air Traffic Management Network Operations","authors":"Z. Chaudhry, K. Fox","doi":"10.1109/ICNS50378.2020.9222889","DOIUrl":"https://doi.org/10.1109/ICNS50378.2020.9222889","url":null,"abstract":"Air Traffic Management (ATM) is under great pressure and facing major challenges in the coming years. The industry is driven by safety, capacity, cost of service, efficiency and the environment. \"Continuous traffic growth, structural airspace and airport capacity issues, and extreme weather events call for new approaches to reshape today’s operations and business models\" [1]. If the aviation industry is to handle the levels of traffic predicted, as well as to cope with new flight modalities on the horizon, including Unmanned Aerial Systems (UAS) and space, \"It will be essential to take a step forward in the capabilities of our systems to cope with the flood of data and to make intelligent decisions\" [2].","PeriodicalId":424869,"journal":{"name":"2020 Integrated Communications Navigation and Surveillance Conference (ICNS)","volume":"46 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2020-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127021426","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 : 2020-09-01DOI: 10.1109/ICNS50378.2020.9222969
Kailin Chen, Shaoyu Wang, Jianfeng Mao
In this paper, we consider predicting travel time for aircraft operated in multi-airport systems by modeling and simulating a multiclass queuing network, which can systematically capture the complicated coupling relationship among multiple airports and terminal airspace and the complex nature of flight trajectories following different traffic flow patterns. In this multiclass queuing network model, each class of queuing network, named a class of customers, is modeled with the data of a traffic flow pattern, which is identified for a cluster of flight trajectories. Airports and airspace sectors are correspondingly modeled as networked servers with nonhomogeneous and time-varying arrival rate, service rate and server capacity to serve those classes of customers following their specific routing probabilities. Then, all of the parameters for setting up the multiclass queuing network model can be properly estimated using historical 4D flight trajectory data. To illustrate the superiority of this model, both average travel time for each class of customers, i.e., aircraft following a particular flow pattern, and the arrival time for an individual flight are predicted via simulations of a multiclass queuing network, and furthermore, compared with the real travel time. A typical example of a multi-airport system, the Guangdong-Hong Kong-Macau Greater Bay Area in China, is utilized to showcase the prediction performance of the proposed multiclass queuing network simulation model. The simulation experiments of the case study demonstrate that the proposed model well fits this multi-airports system. For most of the time periods, the percentage error (PE) of simulated average travel time and real average travel time is less than 5%. The travel time prediction for a random individual flight can achieve around 1% of the percentage error in terms of point estimation.
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