Browse Topic: Air traffic control

Items (281)
This document applies to safety observers or spotters involved with the use of outdoor laser systems. It may be used in conjunction with SAE Aerospace Standard (AS4970) “Human Factors Considerations for Outdoor Laser Operations in the Navigable Airspace.” Additional control measures may be applicable and are listed in ANSI Z136.6.
G10T Laser Safety Hazards Committee
This paper presents a multi-aircraft Markov decision process congestion game to resolve multi-aircraft near midair collisions (NMACs) for small unmanned aerial vehicles (sUAVs). Two key features of this framework are: 1) it leverages the concept of strategic equilibria from game theory to define optimality in multi-aircraft near midair encounters and 2) it extends the existing NMAC metrics to stochastic formulations via the occupancy measure of a Markov decision process. This game-theoretic approach decomposes the classically centralized air traffic control objective to multiple objectives that correspond to each aircraft within the NMAC, and as result, provides an aircraft-centric notion of optimality and safety that is well-suited for distributed conflict resolutions in multi-aircraft NMACs. In addition to modeling multi-aircraft as a game, stochastic metrics that extend the deterministic notions of NMACs are explored. The safety and optimality of the Nash equilibrium multi-aircraft trajectory under a joint NMAC threat is analyzed under different NMAC thresholds and evaluation metrics. Results are simulated numerically for a representative sUAV NMAC geometry.
Wang, JianchaoLi, Sarah
This article addresses the critical need for enhanced weather observation and prediction systems for rotary-wing aircraft. Current weather systems lack granularity in low-altitude airspace, posing safety risks. The application of the ASTM F3673 - 23 Weather Standard Specification is proposed to standardize weather data collection and transition towards a weather sensor performance-based approach rather than instrument certifications, facilitating the deployment of advanced weather sensors. Today, heliports have a binary weather measurement system choice, expensive certified surface weather stations or a windsock. The standard has the potential to change this paradigm, by allowing the deployment of cost-effective digital sensor technology to reduce uncertainty about what is happening at a heliport or vertiport/vertiplex destination. Operationalizing this specification requires rigorous testing and collaboration through public-private partnerships. Bridging the weather educational gap is essential for enhancing safety in low-altitude aviation. Additionally, the integration of Digital Flight Rules (DFR) alongside the ASTM F3673 - 23 Weather Standard presents opportunities for modernizing air traffic management.
Berchoff, DonHarper, ClintZarzar, Chris
6.0.109 - Comparison Study on Fuel Properties of Biodiesel from Jatropha, Palm and Petroleum Based Diesel FuelSAE-PP-002652/4/2021
The increase of air pollution and global warming is a threat for human life. Besides, the price of petroleum is increasing rapidly and the resources are diminishing. This obliged scientists and engineers to look for alternative sources of energy, which are cleaner and more sustainable. Biodiesel, defined as mono-alkyls of esters from vegetable oils and animals fat, is a cleaner renewable fuel and has been considered as the best alternative for petroleum based diesel fuel hence it can be used in any compression ignition engines without any significant modification. The main advantages of using biodiesel are its renewability and better quality of exhaust gas emissions due to their higher content of oxygen. The produce less soot and hence the feed stuck is plant it will regenerate the CO2 by the photosynthesis which ensures the renewability and reduces global warming. But these alternative fuels have faced some obstacles while utilizing in CI engines which are due to some of their physical and chemical characteristics. At this study the fuel properties of jatropha biodiesel and its blends (a non-edible feedstock) were compared with the properties of Palm biodiesel (an edible feedstock) and petroleum based diesel. The viscosity, density, oxidation stability, acid value, water content, iodine value, flash point, pour point, cloud point and calorific value of the samples were analyzed an discussed. The physical properties of the biodiesels are controlled by their chemical properties such as unsaturation level of fatty acids and oxidation stability. Results show that the viscosity of jatropha is higher than palm biodiesel although the density of palm biodiesel is higher. Oxidation stability of the biodiesel has impact on several chemical and physical properties and improvement of oxidation stability can make betterment in these properties. The results of this study will be used as a data backup for another research project.
Mutagaana, Festo
This document sets forth general, functional, procedural, and design criteria and recommendations concerning human engineering of data link systems. The recommendations are based on limited evidence from empirical and analytic studies of simulated data link communication, and on experience from operational tests and actual use of data link. However, because data are not yet available to support recommendations on all potentially critical human engineering issues these recommendations necessarily go beyond the data link research and include requirements based on related research and human factors engineering practice. It is also recognized that evolution of these recommendations will be appropriate as experience with data link accumulates and new applications are implemented. This document focuses primarily on recommendations for data link communications between an air traffic specialist and a pilot, i.e., air traffic services communications, although some recommendations address use of data link for flight information services. Unless otherwise specified within the text, all recommendations apply to both flight deck and ground-based data link systems. This document is intended as a guide for development and evaluation of data link systems. Human engineering considerations are an important element of data link system performance. As illustrated in Figure 1, human engineering recommendations address many component functions required for effective data link communication services in the operational environment. For presentation purposes, the recommendations are divided into five sections: General, functional, procedures, flight deck/air traffic service (ATS) workstation integration, and human-computer interface. To facilitate understanding and use of this document appropriate cross-references to interrelated recommendations appear in parentheses throughout the text.
G-10 Executive Advisory Group
Rotorcrafts are generally subject to a higher fatal accident rate than other segments of aviation, including commercial and general aviation. The safety improvement for rotorcrafts would directly improve the efficiency of air traffic control, since rotorcrafts operate primarily within low-level airspace; an area that is becoming increasingly complex with new entrants, such as unmanned aircraft systems and urban air mobility. The recent impact of artificial intelligence and deep learning algorithms on various aspects of our lives has led to the investigation of the application of these algorithms in the aviation domain; as it may offer a prime opportunity to enhance safety within the aviation community. In this research, we explore the efficacy, reliability, and, more importantly, the explainability of modern deep learning algorithms. We use machine learning models to predict the attitude (pitch and yaw) of rotorcrafts using video data recorded with ordinary cameras. The cameras were mounted inside the helicopter cockpit and recorded outside view through windshield continually during the flight. We train four different architectures of convolutional neural networks (CNNs), i.e., VGG16, VGG19, ResNet50, and Xception. The models achieved 90%, 91%, 88%, and 88%, respectively, average attitude prediction accuracy on the test video dataset. Furthermore, we use gradient class activation maps (grad-CAM) to ascertain the features and regions of the image that influenced the model to make a specific prediction. We show that CNNs learn to focus on similar features as human operators (pilots), i.e., the natural horizon curve. Our findings demonstrate the feasibility of using deep learning models for attitude prediction from f light videos recorded using ordinary inexpensive cameras. The proposed video analytics framework provides a cost-effective means to supplement traditional Flight Data Recorders (FDR); a technology that is often beyond the financial reach of most general aviation rotorcraft operators.
Khan, HikmatJohnson, CharlesBouaynaya, NidhalRasool, GhulamTravis, TylerThompson, Lacey
This SAE Aerospace Standard (AS) covers air data computer equipment (hereinafter designated the computer) which when connected to sources of aircraft electrical power, static pressure, total pressure, outside air temperature, and others specified by the manufacturer (singly or in combination) provides some or all of the following computed air data output signals (in analog and/or digital form) which may supply primary and/or standby flight instruments: Pressure Altitude Pressure Altitude, Baro-Corrected Vertical Speed Calibrated Airspeed Mach Number Maximum Allowable Airspeed Over-speed Warning Total Air Temperature
A-4 Air Data Subcommittee
Self-Affinity of an Aircraft Pilot’s Gaze Direction as a Marker of Visual Tunneling2019-01-18529/16/2019
For the last few years, a great deal of interest has been paid to crew monitoring systems in order to address potential safety problems during a flight. They aim at detecting any degraded physiological and/or cognitive state of an aircraft pilot or crew, such as visual tunneling, also called inattentional blindness. Indeed, they might have a negative impact on the performance to pursue the mission with adequate flight safety levels. One of the usual approaches consists in using sensors to collect physiological signals which are then analyzed. Two main families exist to process the signals. The first one combines feature extraction and machine learning whereas the second is based on deep-learning approaches which may require a large amount of labeled data. In this work, we focused on the first family. In this case, various features can be deduced from the data by different approaches: spectrum analysis, a priori modeling and nonlinear dynamical system analysis techniques including the estimation of the self-affinity of the signals. In this paper, our purpose was to uncover whether the self-affinity of the pilot gaze direction can be related to his cognitive state. To this end, an experiment was carried out on thirteen subjects in a pilot activity representative environment based on a modified version of the software MATB-II. The scenarios were designed to elicit different levels of mental workload eventually associated to attentional tunneling. A database to train the machine learning step was first created by recording the gaze directions of the subjects with an eye-tracker. The self-affinities of these signals were extracted with the Detrended Fluctuation Analysis method. They constituted the inputs of the classifier. Then, other signals were analyzed and classified. Preliminary results showed promising abilities to detect visual tunneling episodes for different levels of mental workload.
Berthelot, BastienMazoyer, PatrickEgea, SarahAndré, Jean-MarcGrivel, ÉricLegrand, Pierrick
The Cloud Detectability Conundrum2019-01-19326/10/2019
Since the beginning of aviation, aircraft designers, researchers, and pilots have monitored the skies looking for clouds to determine when and where to fly as well as when to deice aircraft surfaces. Seeing a cloud has generally consisted of looking for a white / grey puffy orb floating in the sky, indicating the presence of moisture. A simple monitoring of a temperature gauge or dew point sensor was used to help determine if precipitation was likely or accumulation of ice / snow on the airframe could occur. Various instruments have been introduced over the years to identify the presence of clouds and characterize them for the purposes of air traffic control weather awareness, icing flight test measurements, and production aircraft ice detection. These instruments have included oil slides, illuminated rods, vibrating probes, hot wires, LIDAR, RADAR, and several other measurement techniques. Each technology has its own strength and weakness including the particle size range and water content that can be measured and its ability (or lack thereof) to discriminate different types of icing conditions. The FAA release of 14 CFR Part 25 Appendix O and 14 CFR Part 33 Appendix D regulations for SLD and ice crystals has spawned an increased need for detecting and differentiating these icing conditions from the traditional Appendix C clouds. In order to perform these functions, changes to the measurement technologies and flight crew identification methods are needed. To assist ice detector and aircraft manufacturers in the design and certification of systems with these expanded functionalities, an update to ED-103 (AS5498) was recently released. Revision A of this document now provides requirements for the detection and differentiation of Appendix C, O, and D clouds. In 2009, the FAA released Amendment 25-129 which added paragraphs (e) through (h) to § 25.1419 adding focus to the operation of ice protection systems. Amendment 25-140 was released a few years ago adding the Appendix D and O icing environments. While the use of primary and advisory ice detection systems to meet the requirements of § 25.1419 (e) and (g) have steadily increased, the addition of the new icing envelopes has substantially increased the performance demonstrations required. Performance verification is typically performed through icing wind tunnel tests, icing flight tests and comparison to reference instrumentation to show compliance with FAA requirements via the methods described in AS5498A. Demonstrating compliance to these new detection and differentiation requirements over the wide variety of icing conditions presents a significant challenge - particularly as particle sizes increase and water content decreases. The capabilities of facilities and instrumentation used in demonstrating performance have limitations that complicate the evaluation. Some have assumed that an ice detection system failing to meet all expectations would be certified as advisory, giving the flight crew the primary responsibility for detecting icing conditions. This strategy, however, is not clear cut and has its own issues. The discussion herein is intended to shed some light on the certification challenges that exist for verifying the means to detect / differentiate all types of clouds and offers some suggestions on how to resolve this conundrum.
Jackson, Darren Glenn
Currently the VTOL world sees a high number of players investing in electrification, especially coming from the lower end of the market: like commercial drones and startups. Electric engines allow for new architectures and configurations, and partially simplify the design. Simplifying design, lowering cost of development and maintenance, has led to imagine the use of the eVTOL in the passengers' air transportation market, currently reserved to VIP and high net worth individuals. The shift is potentially so radical that a new name has been coined: Urban Air Mobility. This new market is widely imagined as a radical change compared to the current situation: with more traffic, simplified procedures for boarding and in some cases the use of unmanned or remotely piloted vehicles. This leads to the conclusion that the whole transportation system architecture will have to be upgraded or modified to allow for this to happen. Many projects are already running in this direction regarding specific topics, like SESAR JU [1] for Air Traffic Management. This paper treats the Ground Infrastructure, what is commonly referred as Heliport. In the paper a novel architecture envisioned for Urban Air Mobility is proposed and analyzed.
Cacciavillani, EdoardoIelmini, Francesco
A Methodology for Collision Prediction and Alert Generation in Airport Environment2016-01-19769/20/2016
Aviation safety is one of the key focus areas of the aerospace industry as it involves safety of passengers, crew, assets etc. Due to advancements in technology, aviation safety has reached to safest levels compared to last few decades. In spite of declining trends in in-air accident rate, ground accidents are increasing due to ever increasing air traffic and human factors in the airport. Majority of the accidents occur during initial and final phases of the flight. Rapid increase in air traffic would pose challenge in ensuring safety and best utilization of Airports, Airspace and assets. In current scenario multiple systems like Runway Debris Monitoring System, Runway Incursion Detection System, Obstacle avoidance system and Traffic Collision Avoidance System are used for collision prediction and alerting in airport environment. However these approaches are standalone in nature and have limitations in coverage, performance and are dependent on onboard equipment. There is a need to have an integrated solution for collision prediction and alerting to enhance the capacity and operational efficiency of the airports and airspace at the same time ensuring the safety of aircrafts and personnel. This paper proposes a comprehensive, fool proof, integrated solution employing multiple sensor technologies to seamlessly predict collisions in all the zones of airport environment and generate alerts and guidance to prevent the same. Proposed system employs multiple sensor technologies like Optical and Infrared cameras, Laser Range finders, and Primary and Secondary surveillance radars for object monitoring, adopt latest technologies such as advanced image processing, sensor fusion for object detection and path tracking [1], collision prediction and synthetic visual environment for enhanced situational awareness and video based alert generation in real time. Simulation results of a synthesized data analysis that obtained through application of data fusion on multiple data sources and 3D path tracking algorithms are explained in the case study section.
Thupakula, KiranSivaramasastry, AdisheshaGampa, Srikanth
Convective weather systems, i.e., thunderstorms, are the leading cause of flight delay in U.S. airspace. Airline dispatchers must file their flight plans 1 to 2 hours before takeoff, and are often required to incorporate large buffers to forecast weather. Weather changes as flights progress, and airline dispatchers, Federal Aviation Administration (FAA) traffic managers, and air traffic controllers are especially busy during weather events. Workable opportunities for more efficient routes around bad weather are often missed, and automation does not exist to help operators determine when weather avoidance routes have become stale and could be updated to reduce delay.
A Novel Approach to Cooperative and Non-Cooperative RPAS Detect-and-Avoid2015-01-24709/15/2015
A unified approach to cooperative and non-cooperative Detect-and-Avoid (DAA) is a key enabler for Remotely Piloted Aircraft System (RPAS) to safely and routinely access all classes of airspace. In this paper state-of-the-art cooperative and non-cooperative DAA sensor/system technologies for manned aircraft and RPAS are reviewed and the associated multi-sensor data fusion techniques are discussed. A DAA system architecture is presented based on Boolean Decision Logics (BDL) for selecting non-cooperative and cooperative sensors/systems including both passive and active Forward Looking Sensors (FLS), Traffic Collision Avoidance System (TCAS) and Automatic Dependent Surveillance - Broadcast (ADS-B). After elaborating the DAA system processes, the key mathematical models associated with both non-cooperative and cooperative DAA functions are presented. The Interacting Multiple Model (IMM) algorithm is adopted to estimate the state vector of the intruders and this is propagated to predict the future trajectories using a probabilistic model. The analytical models adopted to compute the overall uncertainty volume in the airspace surrounding an intruder are outlined. Based on these mathematical models, the SAA Unified Method (SUM) for cooperative and non-cooperative DAA is presented. In this unified approach, navigation and tracking errors affecting the measurements are considered and translated to unified range and bearing uncertainty descriptors, which apply both to cooperative and non-cooperative scenarios. Simulation case studies are carried out to evaluate the performance of the proposed DAA approach on representative host platforms (AEROSONDE RPAS and typical commercial airliners) and various intruder platforms. Results corroborate the validity of the proposed approach and demonstrate the impact of SUM towards providing a cohesive logical framework for the development of an airworthy DAA capability and a pathway for manned/unmanned aircraft coexistence in all classes of airspace.
Ramasamy, SubramanianSabatini, RobertoGardi, Alessandro
Investigation of GNSS Integrity Augmentation Synergies with Unmanned Aircraft Sense-and-Avoid Systems2015-01-24569/15/2015
Global Navigation Satellite Systems (GNSS) can support the development of low-cost and high performance navigation and guidance architectures for Unmanned Aircraft Systems (UAS) and, in conjunction with suitable data link technologies, the provision of Automated Dependent Surveillance (ADS) functionalities for cooperative Sense-and-Avoid (SAA). In non-cooperative SAA, the adoption of GNSS can also provide the key positioning and, in some cases, attitude data (using multiple antennas) required for automated collision avoidance. A key limitation of GNSS for both cooperative (ADS) and non-cooperative applications is represented by the achievable levels of integrity. Therefore, an Avionics Based Integrity Augmentation (ABIA) solution is proposed to support the development of an Integrity-Augmented SAA (IAS) architecture suitable for both cooperative and non-cooperative scenarios. The performances of this IAS architecture were investigated in representative simulation case studies by testing the ability of the SAA system to exploit the predictive (caution) and reactive (warning) integrity flags generated by ABIA. Additionally, the ABIA False Alarm Rate (FAR) and Detection Probability (DP) performances were examined and an initial evaluation of the complementarity with Space-Based and Ground-Based Augmentation Systems (SBAS/GBAS) was accomplished. Simulation results show that the proposed IAS architecture is capable of performing high-integrity conflict detection and resolution when GNSS is used as the primary source of navigation data and there is a clear synergy with state-of-the art SBAS/GBAS in all applicable flight phases.
Sabatini, RobertoMoore, TerryHill, ChrisRamasamy, Subramanian
Multi-Sensor Data Fusion Techniques for RPAS Detect, Track and Avoid2015-01-24759/15/2015
Accurate and robust tracking of objects is of growing interest amongst the computer vision scientific community. The ability of a multi-sensor system to detect and track objects, and accurately predict their future trajectory is critical in the context of mission- and safety-critical applications. Remotely Piloted Aircraft System (RPAS) are currently not equipped to routinely access all classes of airspace since certified Detect-and-Avoid (DAA) systems are yet to be developed. Such capabilities can be achieved by incorporating both cooperative and non-cooperative DAA functions, as well as providing enhanced communications, navigation and surveillance (CNS) services. DAA is highly dependent on the performance of CNS systems for Detection, Tacking and avoiding (DTA) tasks and maneuvers. In order to perform an effective detection of objects, a number of high performance, reliable and accurate avionics sensors and systems are adopted including non-cooperative sensors (visual and thermal cameras, Laser radar (LIDAR) and acoustic sensors) and cooperative systems (Automatic Dependent Surveillance-Broadcast (ADS-B) and Traffic Collision Avoidance System (TCAS)). In this paper the sensors and system information candidates are fully exploited in a Multi-Sensor Data Fusion (MSDF) architecture. An Unscented Kalman Filter (UKF) and a more advanced Particle Filter (PF) are adopted to estimate the state vector of the objects based for maneuvering and non-maneuvering DTA tasks. Furthermore, an artificial neural network is conceptualised/adopted to exploit the use of statistical learning methods, which acts to combined information obtained from the UKF and PF. After describing the MSDF architecture, the key mathematical models for data fusion are presented. Conceptual studies are carried out on visual and thermal image fusion architectures.
Cappello, FrancescoSabatini, RobertoRamasamy, Subramanian
Integration and Performances Analysis of a Data Distribution Service Middleware in Avionics2015-01-25549/15/2015
The amount of functionalities in modern aircrafts is increasing to satisfy performance, safety and economic benefits. Therefore, the communication needs of avionic systems are growing. Furthermore, the portability and reusability of applications are current challenges of the aerospace industry. The use of the Data Distribution Service (DDS) middleware technology would reduce the complexity of communications and ease the portability and reusability of applications with its standardised interface. Few previous works used a DDS middleware within the aerospace industry and those didn't take into account the impact of this technology on the applications performances. Therefore, this paper presents an impact evaluation of using a DDS middleware on the performances of avionic applications. To do so, a design methodology was proposed to design an automatic flight control system (AFCS) from a high abstraction level representation of a control loop to a low-level implementation on a development board. The AFCS was modeled with Simulink® to control a Boeing 747-400 simulated within the X-Plane flight simulator. The AFCS code was then ported on a Freescale 8572 embedded platform running VxWorks operating system to allow hardware-in-the-loop (HIL) testing. The performances of the AFCS were evaluated through the stabilisation of the aircraft's altitude, speed and roll angle. To measure the impact of using a DDS middleware, the performances of the AFCS with and without a DDS middleware were compared. The results shows that using a DDS middleware allows the aircraft to stabilise at the desired altitude, speed and roll angle without having any significant impact on the performances of the AFCS. However, due to the limitations of this paper's works, there is still much to do before using a DDS middleware in an actual aircraft becomes a common practice.
Landry, KevinBoland, Jean-FrançoisBois, Guy
Automated ATM System Enabling 4DT-Based Operations2015-01-25399/15/2015
As part of the current initiatives aimed at enhancing safety, efficiency and environmental sustainability of aviation, a significant improvement in the efficiency of aircraft operations is currently pursued. Innovative Communication, Navigation, Surveillance and Air Traffic Management (CNS/ATM) technologies and operational concepts are being developed to achieve the ambitious goals for efficiency and environmental sustainability set by national and international aviation organizations. These technological and operational innovations will be ultimately enabled by the introduction of novel CNS/ATM and Avionics (CNS+A) systems, featuring higher levels of automation. A core feature of such systems consists in the real-time multi-objective optimization of flight trajectories, incorporating all the operational, economic and environmental aspects of the aircraft mission. This article describes the conceptual design of an innovative ground-based Air Traffic Management (ATM) system featuring automated 4-Dimensional Trajectory (4DT) functionalities. The 4DT planning capability is based on the multi-objective optimization of 4DT intents. After summarizing the concept of operations, the top-level system architecture and the key 4DT optimization modules, we discuss the segmentation algorithm to obtain flyable and concisely described 4DT. Simulation case studies in representative scenarios show that the adopted algorithms generate solutions consistently within the timeframe of online tactical rerouting tasks, meeting the set design requirements.
Gardi, AlessandroSabatini, RobertoRamasamy, SubramanianMarino, MatthewKistan, Trevor
Augmented Head Mount Virtual Assist for Pilot2015-01-25369/15/2015
Recent years have seen a rise in the number of air crashes and on board fatalities. Statistics reveal that human error constitutes upto 56% of these incidents. This can be attributed to the ever growing air traffic and technological advancements in the field of aviation, leading to an increase in the electronic and mechanical controls in the cockpit. Accidents occur when pilots misinterpret gauges, weather conditions, fail to spot mechanical faults or carry out inappropriate actions. Currently, pilots rely on flight manuals (hard copies or an electronic tablet) to respond to an emergency. This is prone to human error or misinterpretation. Also, a considerable amount of time is spent in seeking, reading, interpreting and implementing the corrective action. The proposed augmented head mount virtual assist for the pilot eliminates flight manuals, by virtually guiding the pilot in responding to in-flight necessities. This is a transparent display unit that eliminates the risk of any misinterpretation by pilot by providing assistance to the pilot in terms of visualization of actions to be taken. It uses either pilot fed data or direct data from the cockpit data system as input, depending on the situation. It can also access necessary flight data and present it to the pilot. An added advantage of the head mount assist other than visualization is that the pilot still retains his field of vision. This paper describes the implementation of the proposed head mount virtual assist for pilots, its advantages over the electronic flight manuals, how it can help reduce or mitigate air fatalities caused due to pilot error and its applications.
Babul Prasad, RinkySiddartha, Vinukonda
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