Aerospace (ISSN 2226-4310) is an international, peer-reviewed, open access journal (free for readers) devoted to the publication of original papers, review articles, short notes and communications related to all fields of aerospace science, engineering and technology, disclosing theoretical, fundamental and applied results linked to potential ap. The Journal of Guidance, Control, and Dynamics also is ranked within the Instruments and Instrumentation category. To simulate a blade out, the containment ring, or containment case, is removed from an engine. Aerospace is a peer-reviewed, open access journal of aeronautics and astronautics published monthly online by MDPI. Central (ARC) is permitted. Special Issue "Advances in Aerospace Sciences and Technology" - MDPI This study. The ability to accurately predict flight time of arrival in real time during a flight is critical to the efficiency and reliability of aviation system operations. An aircraft/engine integrated optimal control method is proposed for turbine-based combined cycle (TBCC) engines based on the Gauss pseudospectral method. interesting to readers, or important in the respective research area. This includes the top-level concept, interface architecture, test results, established operation procedures/timeline, and the summary of the joint rehearsal conducted. In the end, conclusions and observations were formulated resulting from the effects of the work performed during the project. To address this limitation, a generic diagnostic framework is proposed that identifies optimal anomaly detection techniques and data pre-processing and thresholding methods. Two different flames at low and high Reynolds numbers are considered to study the sensitivity of the flame dynamics to turbulence. Columbus, OH 43235; 614-292-5491 Phone; Quick Links. Design and Preliminary Performance Assessment of a PHM System for Electromechanical Flight Control Actuators, A Simulation Framework for Aircraft Take-Off Considering Ground Effect Aerodynamics in Conceptual Design, Design Investigation of Potential Long-Range Hydrogen Combustion Blended Wing Body Aircraft with Future Technologies, Orifice Flow Dynamics in a Rocket Injector as an Excitation Source of Injector-Driven Combustion Instabilities, UAV Platforms for Data Acquisition and Intervention Practices in Forestry: Towards More Intelligent Applications, Space robots exhibit a strong dynamic coupling between the manipulator and the base spacecraft, with this phenomenon being particularly pronounced in mini space robots. In the initial sections of this paper, theoretical issues related to the work being carried out are introduced, and the methodology for creating software for the construction and verification of the aircraft structure along with the need for interchange between databases of generative models is presented. YEAR Impact Factor; 2020-21: 0.53 2019: 0.12 Our study aims to address this by introducing a new approach to calculating the external heat flux of solar radiation that is better suited for uncertainty analysis than previous approaches. Topic Editors: Yongliang Xie, Liang Gong, Change Cai, Topic Editors: Won-Sang Ra, Shaoming He, Ivan Masmitja, Topic Editors: Pedro Resende, Mohsen Ayoobi, Alexandre M. Afonso, Guest Editors: Angelo De Fenza, Mario De Stefano Fumo, Giuseppe Rufolo, Guest Editors: Ashish Vashishtha, Yasumasa Watanabe, Antonella Ingenito, Collection Editors: Sergey Leonov, Kojiro Suzuki, Collection Editors: Carlos Insaurralde, Francesco DellOlio, Collection Editors: Daochun Li, Ting Li, Weizong Wang, Xiaoqiang Li, Zhenxun Gao, Zhihua Wang, Lizhan Bai, Zhan Tu, Collection Editors: Mikhail Ovchinnikov, Dmitry Roldugin, European Aeronautics Science Network (EASN), Adaptive Control of Mini Space Robot Based on Linear Separation of Inertial Parameters, FluidStructure Coupling and Aerodynamic Performance of a Multi-Dimensional Morphing Wing with Flexible Metastructure Skin, Cross-Domain Intelligent Flight Vehicle Design, Integrated Aircraft Design System Based on Generative Modelling, Machine Learning and IoT Trends for Intelligent Prediction of Aircraft Wing Anti-Icing System Temperature, A Data-Light and Trajectory-Based Machine Learning Approach for the Online Prediction of Flight Time of Arrival, Advances in Air Traffic and Airspace Control and Management, Rendezvous and Proximity Operations in Cislunar Space Using Linearized Dynamics for Estimation, Generic Diagnostic Framework for Anomaly DetectionApplication in Satellite and Spacecraft Systems, Efficient Uncertainty Analysis of External Heat Flux of Solar Radiation with External Heat Flux Expansion for Spacecraft Thermal Design, https://doi.org/10.3390/aerospace10080672, Heat Transfer and Cooling Systems for Aerospace Equipment, Combustion Regimes in Turbulent Non-Premixed Flames for Space Propulsion, https://doi.org/10.3390/aerospace10080671, Theoretical, Numerical and Experimental Studies on Clean Energy and Combustion, Low-Thrust Transfer to Quasi-Synchronous Martian Elliptic Orbit via Nonlinear Feedback Control, https://doi.org/10.3390/aerospace10080670, Integrated Conceptual Design and Parametric Control Assessment for a Hybrid Mobility Lunar Hopper, https://doi.org/10.3390/aerospace10080669, Two Hierarchical Guidance Laws of Pursuer in Orbital PursuitEvasionDefense Game, https://doi.org/10.3390/aerospace10080668, Analysis and Suppression of Thrust Trap for Turbo-Ramjet Mode Transition with the Integrated Optimal Control Method, https://doi.org/10.3390/aerospace10080667, Study of Circumferential Grooved Casing Treatment on Cascade Aerodynamic Performance, https://doi.org/10.3390/aerospace10080666, Vortex Flow Phenomena and Physics of Aerospace Engineering Applications, Quadrotor Robust Fractional-Order Sliding Mode Control in Unmanned Aerial Vehicles for Eliminating External Disturbances, https://doi.org/10.3390/aerospace10080665, Cooperative Control, Decision-Making, and Optimization of Unmanned Aerial Vehicles, KARI and NASA JSC Collaborative Endeavors for Joint Korea Pathfinder Lunar Orbiter Flight Dynamics Operations: Architecture, Challenges, Successes, and Lessons Learned, https://doi.org/10.3390/aerospace10080664, Techniques and Science Exploitations for Earth Observation and Planetary Exploration, The Influence of Narrowband Interference on DME System Operation, https://doi.org/10.3390/aerospace10080663, New Trends in Aviation Development 2021-2022, Computational and Experimental Modeling in Magnetoplasma Aerodynamics and High-Speed Gas and Plasma Flows (A Review), https://doi.org/10.3390/aerospace10080662, High Speed Flows: Measurements & Simulations, Flow Structures and Aerodynamic Behavior of a Small-Scale Joined-Wing Aerial Vehicle under Subsonic Conditions, https://doi.org/10.3390/aerospace10080661, Aerodynamic Exploration on Rough Airfoil Based on Overlapping Feathers of a Swift-Wing Structure, https://doi.org/10.3390/aerospace10080660, Structures, Actuation and Control of Morphing Systems, MDPIs Newly Launched Journals in June 2023, Perspectives in Fault Diagnosis and Fault Tolerant Control, Advanced Technologies and Methods in the Energy System, Target Tracking, Guidance, and Navigation for Autonomous Systems, The 4th International Electronic Conference on Applied Sciences (ASEC2023), 13th EASN International Conference on Innovation in Aviation & Space for opening New Horizons, The 10th International Conference on Vortex Flow Mechanics (ICVFM 2023), Advanced Composite Materials and Structures for Aerospace Applications, Recent Advances in Technologies for Aerospace Maintenance, Advanced Method and Technology for Miniaturized Space Application, Latest Advancements in Aeronautics and Astronautics from Beihang University. In such cases, AIAA accepts a license to publish the work and to use it for all of AIAAs Public access mandates are requirements set on all researchers who accept federal grant money.Authors who have accepted federal grants are responsible for depositing permission provided that the original article is clearly cited. The h-index is defined as the maximum value of h such that the given journal/author has published h papers that have each been cited at least h number . their accepted manuscripts into dedicated archives and otherwise complying with agency mandates. It is published by Multidisciplinary Digital Publishing Institute (MDPI). A bibliographic listing with links back to the version of record in Aerospace Research Editors Choice articles are based on recommendations by the scientific editors of MDPI journals from around the world. IEEE Aerospace Conference Proceedings has an h-index of 70.It means 70 articles of this conference and proceedings have more than 70 number of citations. Therefore, the primary effect of turbulence is to increase the fraction of propellants burnt in oxygen-rich and near-stoichiometric conditions. Designing spacecraft involves a careful equilibrium to avoid overengineering or underdesigning, which underscores the importance of employing thermal uncertainty analysis. In the current study, a novel approach based on machine learning (ML) and the Internet of Things (IoT) is proposed to predict the thermal performance characteristics of a partial span wing anti-icing system constructed using the NACA 23014 airfoil section. The uncertainty surrounding the inertial parameters of space robots often renders dynamics-based controllers ineffective, and identifying these parameters in. The journal publishes original papers and review articles related to all fields of aerospace research, in both theory and practice. The final operational orbit has apoares corresponding to the maximum (or minimum) latitude, and nine nodal periods are flown in 5 Martian nodal days. Top journals as determined by Thomson Reuters Journal Impact Factor 2021 Rankings. This journal is devoted to the advancement of the applied science and technology of airborne flight through the dissemination of original archival papers describing significant advances in aircraft, the operation of aircraft, and applications of aircraft technology to other fields. To explore the influence of circumferential grooved casing treatment on subsonic cascade performance, a numerical simulation of subsonic cascade was conducted. Citation Guidelines:This journal was originally published as the Journal of Aerospace Computing, Information, and Communication. This paper proposes a data-light and trajectory-based machine learning approach for the online prediction of estimated time of arrival at terminal airspace boundary (ETA_TAB) and estimated landing time (ELDT), while a flight is airborne. However, at angles of attack smaller than 6, the increase in drag outweighs the increase in lift, leading to lower aerodynamic efficiency for the rough airfoil. At the same time, the exploration system may encounter different types of terrain, requiring an adaptable mobility subsystem able to travel fast on basaltic terrain while avoiding considerable obstacles. Aerospace Science and Technology publishes articles of outstanding scientific quality. the journal. Journal Author | AIAA This journal is devoted to reporting advancements in the science and technology associated with spacecraft and tactical and strategic missile systems, including subsystems, applications, missions, environmental interactions, and space sciences. The impact score (IS) 2021 of International Journal of Aviation, Aeronautics, and Aerospace is 0.83, which is computed in 2022 as per its definition.International Journal of Aviation, Aeronautics, and Aerospace IS is increased by a factor of 0.34 and approximate percentage change is 69.39% when compared to preceding year 2020, which shows a rising trend. Since then, agencies have begun to announce their public access implementation plans, and AIAA is committed to supporting Finally, the paper discusses the challenges and lessons learned from this journey, particularly from the practical FD operational perspectives. Approaches to the control of quasi-stationary separated flows, laminarturbulent transitions, and static and dynamic separation of the boundary layer (for large PA angles of attack) are presented. By decreasing the mode transition time from 60 s to 15 s, the minimum thrust can only increase to 30%, and the thrust trap phenomenon cannot be effectively suppressed. Citation frequencies for individual articles vary greatly and a journals ranking is not indicative of the quality of all articles within My university library is asking me to post my article in their archive; is this permitted? Disclaimer/Publishers Note: The statements, opinions and data contained in all publications are solely AIAA also provides the option for Government authors (and Government contractors, as appropriate) to declare their submissions to be works of the U.S. Government. Connect. The Loire Valley between Sully-sur-Loire and Chalonnes The proposed approach is easy to implement, fast to perform, and effective in prediction, thus presenting an appeal to potential users, especially those interested in flight ETA prediction in real time but having limited data access. A DOI is assigned and the date of publication is available for citation. Journal Rankings on Aerospace Engineering - Scimago Journal & Country Rank Journal of Aerospace Information Systems | AIAA Aerospace Research Central The lunar lava tubes are envisioned as possible hosting structures for a human base in the Moons equatorial regions, providing shelter from radiations, micrometeoroids, and temperature excursion. Moreover, due to the unstable nature of trajectories in cislunar space, it is necessary to design spacecraft that can autonomously make frequent maneuvers to stay on track with a reference orbit. For School of Engineering, University of Glasgow, James Watt Building South, University Avenue, Glasgow G12 8QQ, Scotland, UK. It was found that including thresholding techniques significantly influences the quality of resulting anomaly detection models. The OA article processing charge (APC) is $2400 for immediate open access upon publication. Vous pourrez profiter d'une salle de bains commune, 40 mtres de votre chalet. Aerospace Research Central (ARC) provides access to AIAA Journals, eBooks, Conference Papers and Standards. Typically this is performed by the use of simple thresholds or statistical techniques. Aerospace Engineering Research Resources: High-Impact Journals. Journal of Aerospace Information Systems - SCI Journal Performance & security by Cloudflare. Direct numerical simulations of non-premixed fuel-rich methaneoxygen flames at 20 bar are conducted to investigate the turbulent mixing burning of gaseous propellants in rocket engines. Data-Driven Model to Predict Aircraft Vibration Environment. This Journal is devoted to reporting advancements in the science and technology associated with spacecraft and tactical and strategic missile systems, including subsystems, applications, missions, environmental interactions, and space sciences. The reacting flow is simulated by using an EBI-DNS solver within an OpenFOAM frame. Scimago Journal & Country Rank. SCIMAGO H-index: 47. . bioinformatics, medicine, epidemiology, and radiobiology. Impact Factor: 8.934. It is intended to provide readers of the Journal, with primary interests in propulsion and power, access to papers spanning the range from research through development to applications. The Journal also features Technical Notes regarding recent innovations or applications. In addition, the ThingSpeak platform is applied in this article to realize the concept of the IoT, collect the measured data, and publish the data in a private channel. Our posting policypermits authors to post their accepted conference papers and journal manuscripts on their Cloudflare Ray ID: 7eec714318a4f313 Impact Factor is one of several quantitative tools generated for journals using those of the individual author(s) and contributor(s) and not of MDPI and/or the editor(s). A lockable morphing unit is designed, and its mechanism/structure characteristics, degree of freedom, and the deformable function of its. Research Impact Score*: 2.9.