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A variable-stepsize orbit estimator for real-time spacecraft simulation

A variable-stepsize orbit estimator for real-time spacecraft...

引用

aiaa modeling and simulation technologies conference and exhibit 2003

作者： Hall, J.C. Simulation Systems Space and Satellite Control L3 Communication Systems-West San Jose CA 95134-1619 United States

ISBN: (纸本)9781624100918

The role of estimating algorithms in supplementing real-time numerical propagation of simulated orbits is discussed. An explicit solution for a variable-stepsize, three-point Birkhoff polynomial estimator of order two is exhibited. Advantages of the variable-stepsize approach to real-time simulation of spacecraft orbits are demonstrated by example. Comparative error data for one-, two- and three-point Birkhoff estimators of order two are presented. © 2003 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.

关键词： Orbits

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A system for real-time, closed-loop, multi-spacecraft mission simulation applications

A system for real-time, closed-loop, multi-spacecraft missio...

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aiaa modeling and simulation technologies conference and exhibit 2003

作者： Burns, R.D. Cheung, Cynthia Davis, George Cary, Everett Higinbotham, John Hogie, Keith NASA Goddard Space Flight Center United States Emergent Space Technologies LLC United States Computer Sciences Corp United States

ISBN: (纸本)9781624100918

A mission simulation prototype for Distributed Space Systems has been constructed using existing developmental hardware and software testbeds at NASA's Goddard Space Flight Center. A locally distributed ensemble of testbeds, connected through the local area network, operates in real time and demonstrates the potential to assess the impact of subsystem level modifications on system level performance and, ultimately, on the quality and quantity of the end product science data.

关键词： Testbeds

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Accident kinematics parameter extraction A simulation Tool

Accident kinematics parameter extraction A Simulation Tool

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aiaa modeling and simulation technologies conference and exhibit 2003

作者： Crider, Dennis A. National Resource Specialist-Aircraft Simulation National Transportation Safety Board United States

ISBN: (纸本)9781624100918

This paper outlines the algorithm behind the Safety Board's kinematics parameter extraction code. The Metrojet flight 2710 incident1 will be used as an example of the use of this method when control surface deflections were not recorded. The study of this incident also provides a comparison with the conventional simulation method. The Alaska flight 261 accident2 illustrates the use of the kinematics parameter extraction method when the recorded stabilizer parameter had exceeded the sensor range. This accident also illustrates the adaptation of the basic kinematics code to calculate loads on the stabilizer jackscrew.

关键词： Parameter extraction

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A multi-purpose simulation environment for UAV research

A multi-purpose simulation environment for UAV research

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aiaa modeling and simulation technologies conference and exhibit 2003

作者： Nalepka, Joseph P. Duquette, Matthew M. Air Force Research Laboratory Wright-Patterson AFB OH 45433-7505 United States

ISBN: (纸本)9781624100918

Unmanned aerial vehicles (UAVs) are playing an important role in today's military initiatives. UAVs have proven to be invaluable in locating critical targets and reporting enemy movements or positions to battlefield commanders. Integration of new technologies necessitates simulation prior to fielding new systems in order to avoid costly errors. The unique nature of UAVs in a modern combat environment requires the simulation of a significant part of the battle space to test the robustness of new technologies. Furthermore, simulation environments should be flexible and generic to allow for expedient testing of a wide range of concepts. Members of the Air Force Research Laboratory (AFRL) at Wright-Patterson AFB are developing a multi-purpose simulation environment that will allow for the assessment of many different types of UAV technologies. This paper discusses this simulation activity and describes how it fits into AFRL's corporate plan.

关键词： Antennas

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The framework of distributed interactive simulation for space projects

The framework of distributed interactive simulation for spac...

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aiaa modeling and simulation technologies conference and exhibit 2003

作者： Wang, Hua Tang, Guojin Lei, Yongjun National University of Defense Technology Changsha 410073 China

ISBN: (纸本)9781624100918

Distributed interactive simulation is an innovative technology for the development of space projects. Because of the specific demands for space projects, the basic simulation protocol standard requires additional research and development to become usable in the space domain. Based on the analysis to the entities in the space projects, the framework of distributed interactive simulation for space projects, implementing the High- Level Architecture (HLA) standard and the technology of Object-Oriented simulation (OOS), is developed. The framework is a generic architecture that provides extensible template for applications within space projects. As an application of the framework, the rendezvous and docking distributed interactive simulation system is analyzed. The process of application verifies that building the simulation system based on the framework is conveniently and rapidly. © 2003 by Hua Wang, Guojin Tang and Yongjun Lei.

关键词： Space rendezvous

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An air traffic simulation model that predicts and prevents excess demand

An air traffic simulation model that predicts and prevents e...

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aiaa modeling and simulation technologies conference and exhibit 2003

作者： Boesel, Justin R. McLean VA 22102 United States

ISBN: (纸本)9781624100918

An airplane's ability to absorb delay while airborne is limited and costly. Because of this, the air traffic management system anticipates and manages excessive demand for scarce shared resources, such as arrival runways or busy airspace, so that the delay necessary for buffering can be spread out over a larger distance, or taken on the ground before departure. It is difficult to model these important dynamics in a standard queueresource simulation framework, which does not account for limited delay absorption capacity. The modeling methodology presented here captures these dynamics by employing a large number of independent threads of execution to monitor and enforce a large number of relatively simple mathematical relationships. These relationships calculate feasible time windows for each portion of each flight. The model was implemented in the SLX simulation language. The speed and scalability of SLX are essential to the approach, which would otherwise be impractical. © 2003 by The MITRE Corporation.

关键词： Computer simulation languages

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A feasibility study for ISS and HTV distributed simulation

A feasibility study for ISS and HTV distributed simulation

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aiaa modeling and simulation technologies conference and exhibit 2003

作者： Lauderdale, Grace D. Crues, Edwin Z. Snyder, Danielle V. Hasan, David A. United Space Alliance LLC 600 Gemini M/C USH-483R Houston TX 77058 United States Titan Corporation Astronautics Engineering Unit 1020 Bay Area Boulevard Suite #200 Houston TX 77058 United States

ISBN: (纸本)9781624100918

The United States National Aeronautics and Space Administration (NASA) and Japanese National Space Development Agency (NASDA) are currently investigating the feasibility of a distributed training simulation for Japanese H-II Transfer Vehicle (HTV) operations in the vicinity of the ISS. This paper presents the findings of a study using the Defense modeling and simulation Office's High Level Architecture (HLA) and NASA's Trick simulation Toolkit to implement such a simulation. After introducing the motivation and background for the project, we discuss performance benchmarks and simple distributed simulations we ran using four different implementations of the HLA technology. These technologies look very promising and will be incorporated in the subsequent phases of the ISS/HTV simulation development and most likely in other similar simulation projects. © 2003 by Grace Lauderdale, Edwin Z. Crues, Danielle Snyder and David Hasan.

关键词： NASA

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XNsim extensible network simulation

XNsim extensible network simulation

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aiaa modeling and simulation technologies conference and exhibit 2003

作者： Flannery, Eliot Novotny, John Karpov, Igor Zhang, Chendi Bedrossian, Nazareth S. The Charles Stark Draper Laboratory Inc 2200 Space Park Dr Suite 210 Houston TX 77058 United States Aerospace Systems Group Lead The Charles Stark Draper Laboratory Inc 2200 Space Park Dr Suite 210 Houston TX 77058 United States

ISBN: (纸本)9781624100918

In this paper, a dynamically scalable distributed simulation framework called eXtensible Network simulation (XNsim) is presented. With this approach, a complete simulation can be assembled from shared component subsystems written in different formats, which run on different computing platforms, with different sampling rates, in different geographic locations, and over single/multiple networks. The software uses a peer-to-peer communication architecture. An example is presented to illustrate its features and capabilities Further information about XNsim is available at the product homepage, http://***/. © 2003 by C. S. Draper Laboratory Inc.

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Integrating HLA into the trick simulation development toolkit

Integrating HLA into the trick simulation development toolki...

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aiaa modeling and simulation technologies conference and exhibit 2003

作者： Crues, Edwin Z. Lin, Alexander Hasan, David A. Titan Corporation Astronautics Engineering Unit 1020 Bay Area Boulevard Suite #200 Houston TX 77058 United States NASA Johnson Space Center Automation Robotics and Simulation Division Houston TX 77058 United States

ISBN: (纸本)9781624100918

The increasing size and complexity of simulations presents a number of challenges to engineering organizations, among them: the expense of developing the models and simulation infrastructure and the need to protect proprietary information which might be a crucial part of the simulated systems. To address these challenges, the United States National Aeronautics and Space Administration (NASA) and the Japanese NAtional Space Development Agency (NASDA) are investigating the use of distributed simulation technologies and applying them to a simulation of the International Space Station (ISS) and the Japanese H-II Transfer Vehicle (HTV). The two principal technologies in this work are the Defense modeling and simulation Office's (DMSO) High Level Architecture (HLA) and the NASA Trick simulation Development Toolkit (Trick). This paper presents brief overviews of HLA and Trick, a discussion of the issues associated with incorporating HLA into Trick, an analysis of a standard HLA example application, and a discussion of techniques used to fit the standard example into Trick. Finally, the paper outlines an example time-based dynamic simulation as a simple demonstration of incorporating HLA capabilities into an existing Trick based simulation. © 2003 by Edwin Z. Crues, Alexander Lin, and David Hasan.

关键词： NASA

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The aerospace vehicle technology assessment & simulation (AVTAS) laboratory

The aerospace vehicle technology assessment & simulation (AV...

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aiaa modeling and simulation technologies conference and exhibit 2003

作者： Emsley, Howard T. Hellmann, Gary K. Air Force Research Laboratory Wright-Patterson Air Force Base OH 45433-7505 United States

ISBN: (纸本)9781624100918

The AVTAS Laboratory, located in the Air Force Research Laboratory's Air Vehicles Directorate at Wright-Patterson AFB, Dayton Ohio, is rapidly expanding on its traditional flight control and flying qualities research emphasis by creating simulation Based Research & Development (SBR&D) environments, tools, and processes where researchers and warfighters can assess and evaluate advanced aerospace vehicle technologies and concepts during simulated missions. AVTAS researchers now conduct mission, engagement, and campaign level simulations as needed to demonstrate military utility and to guide/prioritize AFRL investment strategies. Both virtual and constructive simulations1 are used to conduct capabilitybased assessments of AFRL and VA technologies. The AVTAS vision is to quickly and accurately evaluate anything AFRL researchers can imagine and to identify high payoff technology investment paths. Included in this, is the demonstration of the benefits of advanced technology to current and future systems.

关键词： Flight simulators

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