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检索条件"任意字段=AIAA Modeling and Simulation Technologies Conference and Exhibit 2002"

共 282 条记录，以下是91-100 订阅

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Some consequences of UAV design requirements especially on UAV modeling and simulation

Some consequences of UAV design requirements especially on U...

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aiaa modeling and simulation technologies conference and exhibit 2003

作者： Friehmelt, Holger DLR Institute of Flight Systems Lilienthalplatz 7 38108 Braunschweig Germany

ISBN: (纸本)9781624100918

Uninhabited aerial vehicles (UAV) are moving more and more into the limelight of discussion for various military and civil applications. This increasing focus is certainly justified due to obvious advantages of UAVs for dull, dirty and dangerous missions and due to economic advantages by moving the aircrew's tasks to operators on the ground. However, little attention has been spent on the assessment of overall system of systems requirements and their consequences. No means to adequately cover general design requirements with modeling and simulation are therefore given. Early statements about performance, operability cost, and others however are highly desirable already early during the design process. Individual technical requirements have been satisfied in various prototype, demonstrator and initial production programs like Predator, Global Hawk and other international programs. The possible break-through of UAV technology however requires support from the aforementioned awareness of general UAV design requirements and their consequences on design, cost, operation and performance of UAV systems.

关键词： Unmanned aerial vehicles (UAV)

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Automation capabilities analysis methodology for non-controlled airports

Automation capabilities analysis methodology for non-control...

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aiaa modeling and simulation technologies conference and exhibit 2003

作者： Ding, Yuanyuan Rong, Jie Valasek, John Texas A and M University College Station TX 77843-3141 United States Flight Simulation Laboratory Aerospace Engineering Department United States

ISBN: (纸本)9781624100918

Advanced technologies will be needed to enhance and improve the current transportation capabilities of the nation's small aircraft transportation network, and thus help relieve congestion at hub airports. To achieve this goal, current operation concepts and procedures will have to be changed and improved, or perhaps even replaced. This paper proposes a decentralized Air Traffic Management approach, centered on the design of an automated arrival/departure system for non-controlled airports. A hybrid system is introduced that is a fusion of distributed air traffic management and centralized control. A new functional description of the airport terminal area infrastructure named Multi-layer Air Traffic Space is introduced, and automated terminal operations and procedures are addressed. Several types of intelligent agents with negotiation functions are developed in the automation system, and simulation methodology is presented, containing a full hardware and software description. © 2003 by Yuanyuan Ding, Jie Rong and John Valasek.

关键词： Hybrid systems

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eSimDSAT: A web-enabled space station simulation development & analysis tool

eSimDSAT: A web-enabled space station simulation development...

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aiaa modeling and simulation technologies conference and exhibit 2003

作者： Jang, Jiann-Woei Bedrossian, Nazareth Wallace, Johnny Zeigler, Phillip The Charles Stark Draper Laboratory Inc 2200 Space Park Dr Suite 210 Houston TX 77058 United States Rice University Houston TX 77005 United States

ISBN: (纸本)9781624100918

eSim was developed by Draper- Houston to provided a distributed analysis and simulation capability. The Draper Station Analysis Tool (DSAT) is used to solve the problem of the integrated verification of the ISS GN&C system, while meeting demanding schedules and providing confidence in risk estimates. Its functional capabilities include static, frequency domain and time domain analysis. eSimDSAT allows users to access the fully functional version of DSAT via the Internet from anywhere in the world. It is believed that eSimDSAT is the first Web-Enabled Space Station simulation and analysis tool to be reported in the literature. © 2003 by C. S. Draper Laboratory, Inc.

关键词： Space stations

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Virtual simulation set-up for UAVs aerial refuelling

Virtual simulation set-up for UAVs aerial refuelling

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aiaa modeling and simulation technologies conference and exhibit 2003

作者： Pollini, Lorenzo Campa, Giampiero Giulietti, Fabrizio Innocenti, Mario Italy West Virginia University Morgantown WV United States University of Bologna Forli'campus Forli' Italy

ISBN: (纸本)9781624100918

The paper describes the simulation set-up of a virtual benchmark for automatic aerial refuelling of Unmanned Aerial Vehicles (UAVs) using the probe-and-drogue method. A complete virtual environment is created to allow the testing of vision-based algorithms. Autonomous UAV refuelling depends strongly on the capacity of the UAV itself to sense the drogue position;a computer vision system capable of estimating the relative displacement and orientation is presented. The simulation setup uses Commercial Off The Shelf software to create a synthetic environment that can be used to test various vision techniques. This paper will present simulation results with the refueling hose modeled by FEM techniques, simple aircraft dynamics, and a vision technique capable of estimating the drogue position using a set of infrared light emitting diodes (LEDs) similar to those that are usually lit on the drogue itself for nigh time manual refuelling. © 2003 by ***, ***, ***, ***.

关键词： Antennas

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Preliminary model matching of the EMBRAER 170 Jet

Preliminary model matching of the EMBRAER 170 Jet

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aiaa Atmospheric Flight Mechanics conference and exhibit 2003

作者： Cavalcanti, Sergio Papini, Marco OPAL-RT Technologies Montreal Canada

ISBN: (纸本)9781624100895

The development of the EMBRAER 170 Jet has benefited from an expanded modeling and simulation capability at EMBRAER. The aerodynamics model and its accuracy became an important part of the design development phase. This paper discusses the structure of this Simulink model, how the model was matched to flight test, some of the problems encountered, and the advantages and disadvantages of the matching techniques used. RTLAB/ DINAMO, the parameter estimation software used, is also presented. © 2003 by OPAL-RT technologies.

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modeling and simulation framework for multi-objective identification of a guided descending system

Modeling and simulation framework for multi-objective identi...

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aiaa modeling and simulation technologies conference and exhibit 2003

作者： Dobrokhodov, V. Statnikov, R. Department of Aeronautics and Astronautics Naval Postgraduate School Monterey CA 93943-5106 United States

ISBN: (纸本)9781624100918

The paper addresses the task of multi-objective identification of a controllable descending system. The main goal of this work is to develop an optimization framework and technique that can determine feasible and Pareto sets of the numerous uncertainties typical of a parachute-based descending system. The work employs the unique multi-objective optimization method called, the Parameter Space Investigation method. This paper illustrates an advantage of such a technique based on an example of identifying the unknown parameters of the controllable descending system that were discovered during our previous work. Furthermore, it provides a step-by-step implementation of the multi-objective identification of a mathematical model of a controllable circular parachute. The work presents the equations of motion, which are followed by the parameterization of acting aerodynamic forces and moments. It then introduces an application of a twostep parameters identification technique that employs two types of airdrop data (the controlled and uncontrolled set). The paper ends with a summary of the obtained results.

关键词： Parachutes

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A multiple UAV simulation for researchers

A multiple UAV simulation for researchers

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aiaa modeling and simulation technologies conference and exhibit 2003

作者： Rasmussen, Steven Mitchell, Jason W. Schulz, Christopher Schumacher, Corey Chandler, Phillip Veridian Inc Wright-Patterson AFB OH United States Flight Control Division Air Force Research Laboratory Wright-Patterson AFB OH United States

ISBN: (纸本)9781624100918

This paper describes MultiUAV, a simulation that is capable of simulating multiple unmanned aerospace vehicles which cooperate to accomplish a predefined mission. The simulation was constructed using the Mathwork's Simulink simulation software. Construction of the simulation satisfied the need for a simulation environment that researchers can use to implement and analyze cooperative control algorithms. The simulation is implemented in a hierarchical manner with inter-vehicle communication explicitly modeled. During construction of MultiUAV, issues concerning memory usage and functional encapsulation were addressed. MultiUAV includes plotting tools and links to an external program for post-simulation analysis. Each of the vehicle simulations include six-degree-of-freedom dynamics and embedded flight software. The embedded flight software consists of a collection of managers (agents) that control situational awareness and responses of the vehicles. Managers included in the simulation are: Tactical Maneuvering, Sensor, Target, Cooperation, Route and Weapons. © 2003 by the American Institute of Aeronautics and Astronautics, Inc.

关键词： Managers

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Hardware-in-the-loop simulation using open control platform

Hardware-in-the-loop simulation using open control platform

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aiaa modeling and simulation technologies conference and exhibit 2003

作者： Pruett, Stanley H. Slutz, Gary J. Paunicka, James L. Portilla, Eric Air Force Research Laboratory Wright-Patterson Air Force Base OH 45433-7505 United States Protobox LLC Fairborn OH 45324-5551 United States The Boeing Company St. Louis MO 63166-1335 United States Northrop Grumman El Segundo CA 90245-2804 United States

ISBN: (纸本)9781624100918

Air Force Research Laboratory (AFRL) researchers at the Aerospace Vehicle Technology Assessment and simulation (AVTAS) Laboratory are currently conducting the Open Control Platform (OCP) Hardware-In-The-Loop (HITL) project sponsored by the DARPA Software Enabled Control (SEC) Program. The purpose of this project is to develop the capability to be an OCP test-bed and to evaluate the OCP controls and simulation environment for a specific test case. The OCP provides an open, middleware-enabled software framework and development platform for developers of distributed and embedded software applications. The middleware isolates the programmer from the details of the operating system and provides a mechanism for communication with other OCP software components A Traffic Collision Avoidance System (TCAS) was chosen as a representative flight controls application to exercise OCP. The programmatic approach taken by the OCP-HITL project is a series of simulation experiments with increasing complexity. The first simulation was an "all software" simulation, conducted in August 2002. A portion of the "all software simulation" was then migrated to a VME based system running VxWorks. A readiness review of the HITL simulation was conducted in March 2003 in preparation for the actual testing scheduled for the May 2003 timeframe. This readiness review tested a 2 ship non-co-operating scenario, a 2 ship cooperating scenario, and a pilot-in-the-loop scenario. Future testing is planned.

关键词： Middleware

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Aircraft simulation techniques used in low-cost, commercial software

Aircraft simulation techniques used in low-cost, commercial ...

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aiaa modeling and simulation technologies conference and exhibit 2003

作者： Zyskowski, Michael K. Microsoft Corporation Redmond WA United States

ISBN: (纸本)9781624100918

The simulation of aircraft is probably one of the most complicated yet exciting fields in the engineering world today. As personal computers have become more powerful, the ability to simulate the complex behavior of aircraft motion in real time is now possible on these lower-cost platforms. Microsoft Flight Simulator is one of the most mature, low-cost and feature-packed simulation programs on the market today;Microsoft Combat Flight Simulator includes many of the same simulation capabilities available in Microsoft Flight Simulator. Through implementation of the classical aircraft Equations of Motion, Quaternion Transformation methods, Direct Cosine Euler Transformations and non-dimensional aerodynamic coefficient implementation, these programs provide a robust and accurate aircraft simulation software package that have been built, added to and improved upon through years of development. Together with the detailed propulsion simulation techniques, ground reaction fidelity and abundance of systems modeling, these mainstays of the marketplace offer many unique aircraft simulation features. This paper will provide a brief product history and describe the techniques used to simulate aircraft in both Microsoft Flight Simulator and Microsoft Combat Flight Simulator. © 2003 by Michael K. Zyskowski and Microsoft Corporation.

关键词： Flight simulators

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Development of a simulation S/W for evaluation of precision auto-landing algorithms for unmanned aerial vehicles

Development of a simulation S/W for evaluation of precision ...

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aiaa modeling and simulation technologies conference and exhibit 2003

作者： Sugjoon, Yoon Jun-Seok, Lim Kang-Soo, Kim Jae-Joon, Ahn Dept. of Aerospace Engineering Sejong University Seoul Korea Republic of

ISBN: (纸本)9781624100918

A simulation S/W is developed to evaluate performances of MLS (Microwave Landing System) and IBLS (Integrated Beacon Landing System) in precision auto-landing. For this study classical PID and optimal LQG controllers are developed as well as mathematical models of MLS and IBLS. Ship-landing condition is also considered by assuming sinusoidal movement of the ship in the pitch direction. The simulated aircraft is F-16 in the study of precision auto-landing. For the integrated simulation environment GUI windows are designed for input of parameter values necessary for simulation, such as vehicle performance and environmental data. For validation and verification of models various comparison graphs of simulation outputs are comprised in the GUI design as well as 3D visual simulation of vehicle dynamics. Numerous numerical tests of IBLS and MLS show that they satisfy the requirements of CAT III precision autolanding in the presence of moderate disturbances when they are combined with either classical or optimal controllers. © 2003 by the American Institute of Aeronautics and Astronautics, Inc.

关键词： Vehicle performance

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