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Improving the aircraft design process using Web-based modeling and simulation
2000
ACM Transactions on Modeling and Computer Simulation
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Designing and developing new aircraft systems is time-consuming and expensive. ...
An object-oriented framework is a set of classes that embodies an abstract design for solutions individual frameworks for the visual assembly interface, persistence engine, connection services, simulation ...
The integration of object technology represents a fundamental (some would NASA Center for AeroSpace Information Computational presents our vision of an aircraft design process using Web-based modeling ...
doi:10.1145/353735.353739
fatcat:m6q5n2hi3vhm3f5l4kcp2hfgta
Methodologies for the Synthesis of Reliable MEA Electrical Power System Architectures
2020
2020 IEEE Vehicle Power and Propulsion Conference (VPPC)
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This paper reviews the main optimization approaches and design frameworks found in the literature for the synthesis of power system architectures for More Electric Aircraft (MEA). ...
Being safety the most important feature, it is imperative to explore the benefits these design approaches can offer in the formulation of a MEA power system design problem considering safety and reliability ...
MEA EPS with novel design frameworks considering the integration of computation, communication, and control into a highly integrated system. ...
doi:10.1109/vppc49601.2020.9330868
fatcat:msfhbu4lrzbefexslo5krhrawm
Multidisciplinary Conceptual Design Optimization of Space Transportation Systems
1999
Journal of Aircraft
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An important goal of the aerospace community is to develop the capability to design and optimize systems for life-cycle cost estimation. ...
Computational Frameworks
To perform multidisciplinary vehicle synthesis and optimi- zation on conceptual space transportation systems, designers rely on computer-based simulation and analysis tools. ...
doi:10.2514/2.2428
fatcat:ofndy4boi5h3xbfieatxndgl7a
Web-Based Integrated Research Environment for Aerodynamic Analyses and Design
[chapter]
2009
Future Application and Middleware Technology on e-Science
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e-AIRS [1, 2] , an abbreviation of 'e-Science Aerospace Integrated Research System,' is a virtual organization designed to support aerodynamic flow analyses in aerospace engineering using the e-Science ...
The present paper describes those services and the internal architecture of the e-AIRS system. ...
Acknowledgments The current work is a product of 'Development of e-Science technology for fluid dynamic research in various fields' project. ...
doi:10.1007/978-1-4419-1719-5_1
fatcat:cpzyzsrlm5earp3nrd2nhjfuwe
Multi-Platform Atmospheric Sounding Testbed (MAST)
[chapter]
2010
Aerospace Technologies Advancements
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The SOX system utilizes MySQL relational database manager for distributed database service and Mono for execution of the .NET framework on Linux platforms. ...
OSSE System The OSSE System simulates an atmospheric sounder by integrating three types of models, a forward model for the physical properties of the atmosphere, an instrument model for measurement quality ...
The research described in this paper was carried out at the Jet Propulsion Laboratory, California Institute of Technology, under a contract with the Advanced Information System Technology (AIST) program ...
doi:10.5772/6931
fatcat:xutirt5adncgrgkic4ajkaxf3m
CADAC: Multi-use Architecture for Constructive Aerospace Simulations
2011
The Journal of Defence Modeling and Simulation: Applications, Methodology, Technology
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The simulation framework Computer Aided Design of Aerospace Concepts (CADAC) has its roots in FORTRAN code that dates back to the 1960s and was used by industry and the U.S. ...
In the 10 years of development, CADAC++ based constructive simulations have been built for many types of aerospace vehicles and integrated with mission-level simulations. ...
Propulsion data are tailored to the type of propulsion system. For rocket motors, simple thrust tables may suffice. ...
doi:10.1177/1548512910395641
fatcat:olfffm7rdjbw3ed5iicmyyoonm
The Jet Propulsion Library: Modeling and simulation of aircraft engines
2017
Proceedings of the 12th International Modelica Conference, Prague, Czech Republic, May 15-17, 2017
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The Jet Propulsion Library is a new Modelica library that provides a foundation for modeling and simulation of jet engines, and the model-based design of integrated aircraft systems. ...
It provides a fully rigorous foundation for sizing and performance computations, and provides a number of advantages over existing domain-specific solutions due to the use of the Modelica language. ...
We acknowledge the contributions of Shashank Swaminathan who contributed to the interface and template structure described in section 2.6 as summer intern at Modelon, Inc in 2016. ...
doi:10.3384/ecp17132909
dblp:conf/modelica/SielemannPSS17
fatcat:7jrwqnwxjraqlphudpbau7cwjy
Usando Simulación en los Sistemas Astronáuticos y Aeroespaciales
Using Simulation in Astronautic and Aerospace Systems
2013
Revista Espacio I+D Innovación más Desarrollo
Using Simulation in Astronautic and Aerospace Systems
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For our purposes, Computing covers innovative approaches to flight and ground computing that have the potential to increase the robustness of future aerospace systems and the science return on long-duration ...
TA11-1 DRAFT exeCuTive Summary Figure 1 is an initial draft strategic roadmap for the Modeling, Simulation, Information Technology and Processing Technology Area. ...
Towards this objective, architecture frameworks have been established as a guide for the development of architectures. ...
doi:10.31644/imasd.2.2013.a02
fatcat:zu6cgc7hv5bkvghghefcaqvyri
Special Issue Editorial: Robotics: Mechanics and Control of Locomotion
2017
Journal of nonlinear science
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Variational calculus is leveraged to establish a control-oriented mathematical formulation, which is illustrated through numerical simulations. Computational analysis Communicated by ...
The collection of articles is largely focused around the mechanics and control of locomotion, an exemplary domain where nonlinear science naturally meets robotics. ...
Last, but not least, the work by Mummolo et al. presents a computational framework for the estimation of balanced and falling states of legged systems. ...
doi:10.1007/s00332-017-9387-0
fatcat:xgjj6mwkjvc2xbxskdwaupjl4a
Evolutionary algorithms to optimize low-thrust trajectory design in spacecraft orbital precession mission
2017
2017 IEEE Congress on Evolutionary Computation (CEC)
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However, in addition to the orbital perturbation acting on the spacecraft, a number of parameters related to the spacecraft and its propulsion system must be optimized. ...
With a unique trajectory model, EAs prove to be an efficient, reliable and versatile optimization solution, capable of being implemented in conceptual and preliminary design of spacecraft for orbital precession ...
One solution for this problem is using electric propulsion systems to correct the direction of the space orbit apse-line. ...
doi:10.1109/cec.2017.7969517
dblp:conf/cec/ShiraziCL17
fatcat:xjrisagpfrecvkah5jc36wzzyq
Mission Reliability Simulation Method of Ship Propulsive System
2018
DEStech Transactions on Computer Science and Engineering
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An object-oriented hierarchical and modular simulation method was used to decompose the task process into several sub-processes according to the task target. ...
And then through the modeling of internal running rules of sub-processes, a mission reliability simulation model of a complex repairable ship propulsive system with multitask process and multiuse state ...
Acknowledgment This work was supported by the Youth Foundation of Naval University of Engineering under Grant No. 425517K155. ...
doi:10.12783/dtcse/amms2018/26220
fatcat:thfvzb2hv5fezmclhbrnnhv2q4
Schedule and Program
2020
2020 IEEE Aerospace Conference
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9:45
AM
3.0501 Miniaturized and
Reconfigurable RF
Electronics Architecture
for SmallSat Applications -
Fernando Aguirre
10.0105 Computational
Framework for the Study
of Infectious Disease ...
Today, we sample an image and then act on it using a computer. ...
doi:10.1109/aero47225.2020.9172334
fatcat:qosbpgtqnvckdhkjzvtxzqgw3i
An architecture and a methodology for intelligent control
1996
IEEE Expert
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The canonical form within this framework facilitates an open and scalable system architecture. The well-defined structures facilitate efficient knowledge engineering processes. ...
We outline a multiple dimensional reference model architecture and a methodology for representing and developing intelligent systems. ...
Fitzgerald, Nat Frampton, Philip Feldman, and Clyde Findley of the Advanced Technology Corporation have participated in various stages of the submarine project. ...
doi:10.1109/64.491281
fatcat:jgzo4hsqsrd3hi33ctnrfh2fti
Variable Fidelity Conceptual Design Environment for Revolutionary Unmanned Aerial Vehicles
2008
Journal of Aircraft
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The propulsion module, Fig. 3, step 5, includes six propulsion architectures combining power systems, propulsive systems, and power management and distribution (PMAD) systems. ...
*Boeing Professor of Advanced Aerospace Systems Analysis and Director of Aerospace Systems Design Laboratory, Daniel Guggenheim School of Aerospace Engineering. Associate Fellow AIAA. ...
doi:10.2514/1.35567
fatcat:gyiq3ry4rbdylpwdnvc6dbbd4q
A Platform for Autonomous Path Control of Unmanned Airship
2017
Journal of Aeronautics & Aerospace Engineering
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Prove this concept all kinematics and dynamics of a light than air vehicle (blimp) is develop; a prototype of an embedded parallel distributed compute was constructed; and new procedures to resolve navigations ...
The new evasion procedures were implemented into a simulator and a new parallel/distributed program for optimal path discover was developed to be used into the cluster prototype. ...
The new framework The frame work proposed in this article is composed of an embedded parallel distributed computer, a new collision evasion system, a parallel distributed mission route generator program ...
doi:10.4172/2168-9792.1000190
fatcat:23xuklbkzzbcbf7estfig3mr4q
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