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Development of a real-time virtual airspace simulation capability for air traffic management research

Development of a real-time virtual airspace simulation capab...

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aiaa modeling and simulation technologies conference and exhibit 2002

作者： Sullivan, Barry T. Malsom, Scott J. NASA-Ames Research Center United States

ISBN: (纸本)9781624101212

This paper describes the NASA Ames Research Center's effort to develop a real-time human-in-the-loop Air Traffic Management (ATM) simulation capability that will emulate operations within the National Airspace System. This unique capability will be used to evaluate the human performance impact of ATM concepts at both the systems and local levels with the requisite degrees of fidelity. This new Virtual Airspace simulation Technology (VAST) will examine critical core component technologies and candidate system level concepts and architectures to meet the requirements of the air transportation system of the future. The goal of this new capability is to provide human-in-the-loop simulations of operations within the NAS to never before achieved levels of fidelity. This capability will also provide a safe, cost effective, common, flexible and accessible platform for evaluating futuristic ATM concepts. © by the American Institute of Aeronautics and Astronautics, Inc.

关键词： NASA

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A multi-operator simulation for investigation of distributed air traffic management concepts

A multi-operator simulation for investigation of distributed...

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aiaa modeling and simulation technologies conference and exhibit 2002

作者： Peters, Mark E. Ballin, Mark G. Sakosky, John S. Seagull Technology Hampton VA 23666 United States NASA Langley Research Center Hampton VA 23666 United States SAIC Hampton VA 23666 United States

ISBN: (纸本)9781624101212

This paper discusses the current development of an air traffic operations simulation that supports feasibility research for advanced air traffic management concepts. The Air Traffic Operations simulation (ATOS) supports the research of future concepts that provide a much greater role for the flight crew in traffic management decision-making. ATOS provides representations of the future communications, navigation, and surveillance (CNS) infrastructure, a future flight deck systems architecture, and advanced crew interfaces. ATOS also provides a platform for the development of advanced flight guidance and decision support systems that may be required for autonomous operations. © 2002 by the American Institute of Aeronautics and Astronautics, Inc.

关键词： Decision support systems

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Virtual reality modeling simulation of the Re-entry motion of an axialsymmetric vehicle

Virtual reality modeling simulation of the Re-entry motion o...

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aiaa modeling and simulation technologies conference and exhibit 2002

作者： Guidi, A. Chu, Q.P. Mulder, J.A. Nicolosi, F. Delft University of Technology Delft Netherlands University of Naples Federico II Naples Italy

ISBN: (纸本)9781624101212

This work started during the stability analysis of the Delft Aerospace Re-entry Test demonstrator (DART) which is a small axisymmetric ballistic re-entry vehicle. The dynamic stability evaluation of an axisymmetric re-entry vehicle is especially concerned on the behaviour of its angle of attack during the flight through the atmosphere. The variation in the angle of attack is essential for prediction of the trajectory of the vehicle and for heating requirement of the structure of the vehicle. The concept of the total angle of attack and the windward meridian plane are introduced. The position of the centre of pressure can be a crucial point in the stability of the vehicle. Although the simpleness of an axisymmetric shape, the re-entry of such a vehicle is characterised by several complex phenomenologies that were analysed with the aid of the flight simulator and of a 3D virtual reality modeling simulator. © 2002 by the author(s). Published by the American Institute of Aeronautics and Astronautics, Inc.

关键词： Angle of attack

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Accident simulation through radar: Two case studies

Accident simulation through radar: Two case studies

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aiaa modeling and simulation technologies conference and exhibit 2002

作者： Crider, Dennis A. Aircraft Simulation National Transportation Safety Board

ISBN: (纸本)9781624101212

Aircraft simulation is a powerful tool for accident investigation. For cases where the number of flight data recorder (FDR) parameters are limited, the Safety Board has used simulation and its inverse (kinematics extraction) to extract non-recorded control time histories from aircraft motion. For cases where there is radar data but no FDR data, simulation can eliminate some failures from the list of possible causes and can be used to find control time histories that do match the accident. An example of this is seen in the study of the Silkair MI185 accident. In the investigation of the THY flight 5904 accident, only short segments of FDR tape were recovered. A simulation was done that matched the FDR data during the times when FDR data was available and flew through radar data during time periods between FDR tape segments.

关键词： Tape recorders

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Building multi-UAV simulation methods

Building multi-UAV simulation methods

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aiaa modeling and simulation technologies conference and exhibit 2002

作者： Lluch, Daniel The MathWorks Natick MA United States

ISBN: (纸本)9781624101212

The objective of this paper is to show a complete simulation of multiple Unmanned Air Vehicles (UAVs), with emphasis on the requirements needed and the benefits realized in making the simulation functional for an arbitrary number of vehicles. Cooperative control will be shown for an autonomous set of UAV in performance of some task, such as formation, reconnaissance, surveillance, search, jamming, decoy, or target attack. The simulation is developed using a Commercial Off-the-Shelf (COTS) software package that allows for a hierarchical block diagram representation to include the control laws and vehicle models. The tools also allow for the use of finite state machines to be used for control law modes. Visualization is achieved by having the simulation drive a VRML (Virtual Reality modeling Language) virtual world allowing the interactions of the vehicles in their environment to be seen as the simulation is running. The simulation also will allow for replacement of certain components;such as the control scheme that is used or the vehicles that are modeled. The basis of this simulation comes from previous research performed in the study of aircraft formation flight in the context of cooperative game theory and the natural aggregate motion of flocking birds, schooling fish, and herding of land animals. © 2002 by the author(s). Published by the American Institute of Aeronautics and Astronautics, Inc.

关键词： Flight simulators

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A multi-fidelity simulation environment for human-in-the-loop studies of distributed air ground traffic management

A multi-fidelity simulation environment for human-in-the-loo...

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aiaa modeling and simulation technologies conference and exhibit 2002

作者： Prevot, Thomas Palmer, Everett Smith, Nancy Callantine, Todd San Jose State University NASA Ames Research Center Mail Stop 262-4 Moffett Field CA 94035-1000 United States

ISBN: (纸本)9781624101212

This paper describes a Distributed Air Ground Traffic Management (DAG-TM) simulation environment created at NASA Ames Research Center for conducting human-in-the-loop evaluations of new concepts for managing and controlling air traffic. The simulation environment combines high fidelity full mission flight simulators with mid-fidelity air traffic controller/manager workstations as well as low to mid-fidelity desktop workstations for additional pilots, controllers, experiment managers and observers. The simulation is distributed amongst different facilities and laboratories at Ames and provides for connecting multiple off-site simulators via the Internet. The Crew Activity Tracking System (CATS) can be attached for real-time tracking and analysis of pilot and controller activities, and intelligent agents can supplant ancillary human participants. © 2002 by the American Institute of Aeronautics and Astronautics, Inc.

关键词： Flight simulators

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Flight simulation for the development of an experimental UAV

Flight simulation for the development of an experimental UAV

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aiaa modeling and simulation technologies conference and exhibit 2002

作者： Johnson, Eric N. Mishra, Sumit School of Aerospace Engineering Georgia Institute of Technology Atlanta GA 30332-0150 United States

ISBN: (纸本)9781624101212

The use of flight simulation tools to reduce the schedule, risk, and required amount of flight testing for complex aerospace systems is a well-recognized benefit of these approaches. However, some special challenges arise when one attempts to obtain these benefits for the development and operation of an Experimental Uninhabited Aerial Vehicle (UAV) system. These types of UAV systems are characterized by the need for the need for continual checkout of experimental software and hardware. Also, flight-testing can be further leveraged by complementing research results with flight-test validated simulation results for the same experimental UAV. In this paper, flight simulation architectures for system design, integration, and operation of an experimental helicopter-based UAV, the GTMax, are explored, and the development of a simulation tool described. The chosen helicopter-based UAV platform (a Yamaha R-Max) is well instrumented: differential GPS, inertial measurement unit, sonar altimeter, radar altimeter, and a 3-axis magnetometer. One or two flight processors can be utilized.

关键词： Antennas

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Generic pilot and flight control model for use in simulation studies

Generic pilot and flight control model for use in simulation...

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aiaa modeling and simulation technologies conference and exhibit 2002

作者： Johnson, Eric N. Pritchett, Amy R. School of Aerospace Engineering Georgia Institute of Technology Atlanta GA 30332-0150 United States

ISBN: (纸本)9781624101212

In developing an aircraft simulation, a number of aircraft dynamic models are available with a range of fidelity. However, many applications of simulation also require a model of the flight control or of the pilot to realize their goals. These models can be difficult to implement using classical control methods and, in the case of flight control systems, may not be publicly available. This paper describes a generic pilot and flight control model suitable for many applications of simulation in research and design. This model may be easily implemented in simulation by using a architecture adapted from adaptive control for innerloop attitude control, which capitalizes upon the dynamic information known within a simulation to create a stable control behavior. This architecture allows specification of the closed-loop behavior of the aircraft and controller (pilot or autopilot). Specific implementations of inner- and outer-loop control behavior are detailed. simulation runs with this controller, acting as both a pilot and as a flight control system, are documented. © 2002 by the author(s). Published by the American Institute of Aeronautics and Astronautics, Inc.

关键词： Flight control systems

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Flight simulation model development and validation for the JPATS ground based training system

Flight simulation model development and validation for the J...

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aiaa modeling and simulation technologies conference and exhibit 2002

作者： Kimball, Dwayne Hurtig Jr., L. Anthony Galloway, R. Thomas Stability and Control Raytheon Aircraft Company Raytheon Aircraft Company NAWCTSD

ISBN: (纸本)9781624101212

This paper describes the development and validation of the flight simulation model used in the flight simulators of the Joint Primary Air Training System. This model extends to the full maneuvering envelope of the aerobatic T-6A primary training aircraft, and includes the aircraft's aerodynamics, propulsion and flight control systems, and mass properties. Model requirements and validation tolerances are discussed, as well as the unconventional procurement process employed and certain differences in approach between civilian and military cultures which were successfully bridged. Data sources including wind tunnel, air vehicle flight testing and simulation-specific flight tests are described, as is the model's formulation and the desktop simulation and data manipulation tools that contributed to the efficiency of the effort and to the model's fidelity. Finally, the model validation process is detailed, and the test and evaluation phase summarized.

关键词： Training aircraft

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Integrated solution for aircraft data visualization and simulation image generation

Integrated solution for aircraft data visualization and simu...

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aiaa modeling and simulation technologies conference and exhibit 2002

作者： Heise, M. Holzapfel, F. Sachs, G. Institute of Flight Mechanics and Flight Control Technische Universität München Munich Germany

ISBN: (纸本)9781624101212

Modern software and hardware solutions available for engineering flight simulation are divided in commonly distributed desktop data and aircraft visualization and high fidelity image generators for pilot-inthe- loop simulation. Recent performance improvements in computer hardware, especially the availability of affordable 3D accelerated graphics boards, allow high-quality real-time three-dimensional visualization of aircraft motion, configuration as well as environment variables. Thus the recent 3D hardware trends tend to facilitate in achieving realistic simulation on desktop computers. The presented system unifies and incorporates both aspects of accurate realtime data visualization and aircraft representation as well as high fidelity realistic multi-channel image generation for flight simulation. Both objectives are delivered in a single uniform software solution with a communication module for data exchange aimed at achieving high-level performance on low-cost 3Daccelerated desktop computers. © 2002 by the author(s). Published by the American Institute of Aeronautics and Astronautics, Inc.

关键词： Data visualization

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