检索结果-内蒙古大学图书馆

您好，读者！请登录

内蒙古大学图书馆

首页
概况
党建
资源
服务
科研支持
- 论文收录引用证明
- 科技查新
知识产权
档案馆
帮助

咨询与建议

建议与咨询留下您的常用邮箱和电话号码，以便我们向您反馈解决方案和替代方法

您的常用邮箱：*

您的手机号码：*

问题描述：

当前已输入0个字，您还可以输入200个字

全部搜索
期刊论文
图书
学位论文
标准
纸本馆藏
外文资源发现
数据库导航
超星发现

高级检索

时间限定

出版年份：

文献类型

图书期刊文献学位论文多媒体

馆藏选择

电子馆藏纸本馆藏

核心期刊

全部期刊 SCI 收录期刊 SSCI 收录期刊 EI 收录期刊 CSCD 收录期刊 CSSCI 收录期刊

语言

中文英文

文献类型

期刊文献图书学位论文标准纸本馆藏

帮助

文字说明：

T=题名（书名、题名），A=作者（责任者），K=主题词，P=出版物名称，PU=出版社名称，O=机构（作者单位、学位授予单位、专利申请人），L=中图分类号，C=学科分类号，U=全部字段，Y=年（出版发行年、学位年度、标准发布年）

检索规则说明：

AND代表“并且”；OR代表“或者”；NOT代表“不包含”；(注意必须大写,运算符两边需空一格)

检索范例：

范例一：(K=图书馆学 OR K=情报学) AND A=范并思 AND Y=1982-2016
范例二：P=计算机应用与软件 AND (U=C++ OR U=Basic) NOT K=Visual AND Y=2011-2016

分类表

所选分类

>> <<

限定检索结果

文献类型

277 篇 会议
5 篇 期刊文献

馆藏范围

282 篇 电子文献
0 种 纸本馆藏

日期分布

学科分类号

264 篇 工学
- 163 篇 航空宇航科学与技...
- 143 篇 计算机科学与技术...
- 129 篇 软件工程
- 68 篇 力学（可授工学、理...
- 55 篇 控制科学与工程
- 34 篇 交通运输工程
- 27 篇 机械工程
- 24 篇 土木工程
- 23 篇 建筑学
- 20 篇 电子科学与技术（可...
- 18 篇 动力工程及工程热...
- 17 篇 信息与通信工程
- 14 篇 电气工程
- 14 篇 化学工程与技术
- 11 篇 安全科学与工程
- 5 篇 仪器科学与技术
- 4 篇 材料科学与工程（可...
- 4 篇 船舶与海洋工程
- 3 篇 石油与天然气工程
117 篇 理学
- 67 篇 数学
- 48 篇 物理学
- 17 篇 统计学（可授理学、...
- 15 篇 系统科学
- 11 篇 化学
- 7 篇 大气科学
- 3 篇 生物学
49 篇 管理学
- 46 篇 管理科学与工程(可...
- 36 篇 工商管理
19 篇 经济学
- 19 篇 应用经济学
19 篇 军事学
4 篇 法学
- 4 篇 社会学
2 篇 教育学
2 篇 医学
1 篇 农学

主题

33 篇 flight simulator...
15 篇 nasa
8 篇 air traffic cont...
5 篇 computational fl...
4 篇 gas turbines
4 篇 antennas
4 篇 airports
3 篇 launch vehicles
3 篇 matlab
3 篇 turbulence model...
3 篇 wind tunnels
3 篇 angle of attack
3 篇 flight control s...
3 篇 personal compute...
3 篇 hardware-in-the-...
3 篇 actuators
2 篇 propellants
2 篇 acoustic fields
2 篇 closed loop syst...
2 篇 internet protoco...

机构

10 篇 delft university...
8 篇 control and simu...
5 篇 school of aerosp...
5 篇 the charles star...
4 篇 nasa langley res...
3 篇 texas a and m un...
3 篇 nasa ames resear...
3 篇 delft university...
3 篇 raytheon missile...
3 篇 mclean va 22102 ...
3 篇 unisys corporati...
3 篇 titan corporatio...
2 篇 embraer - empres...
2 篇 systems developm...
2 篇 naval air system...
2 篇 air force resear...
2 篇 the space roboti...
2 篇 defence research...
2 篇 nasa glenn resea...
2 篇 department of ae...

作者

11 篇 mulder m.
10 篇 van paassen m.m.
6 篇 madden michael m...
6 篇 glaab patricia c...
6 篇 leslie richard a...
6 篇 cunningham kevin
6 篇 geyer david w.
5 篇 bezdek william j...
5 篇 zaal p.m.t.
4 篇 kenney p. sean
4 篇 pollini lorenzo
4 篇 pool d.m.
4 篇 johnson eric n.
4 篇 chu q.p.
4 篇 crues edwin z.
3 篇 khorrami mehdi r...
3 篇 advani s.k.
3 篇 manikonda vikram
3 篇 mulder j.a.
3 篇 valasek john

语言

282 篇 英文

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101-110 订阅

全选清除本页清除全部题录导出标记到"检索档案"

详细简洁

排序：

A synthetic environment for simulation of vision-based formation flight

A synthetic environment for simulation of vision-based forma...

引用

aiaa modeling and simulation technologies conference and exhibit 2003

作者： Pollini, Lorenzo Mati, Roberto Innocenti, Mario Campa, Giampiero Napolitano, Marcello Italy West Virginia University Morgantown WV United States

ISBN: (纸本)9781624100918

This paper describes the design of autopilots and formation control laws and then the simulation setup and the first results of a novel architecture for close formation flight based on computer vision. The reference aircraft model is the West Virginia University YF-22 model aircraft. The simulation setup includes aircraft dynamics, autopilots and formation keeping controller and a module that creates a synthetic environment for the simulation of the vision equipment based on a commercial software called Dyna- WORLDS. DynaWORLDS is capable of generating synthetic images as if were captured by the camera onboard the wingman. Uniquely identifiable infrared light markers (light emitters each with different wavelength) are applied to the Leader aircraft and a recent iterative, globally convergent, pose estimation algorithm (LHM) is adopted to reconstruct the leader position and attitude. The formation control laws, designed with GPS measurements in mind, have been applied successfully with the Leader position, velocity and Heading estimates obtained from the vision system alone. A more feasible and less expensive solution using light markers with unique wavelength is then introduced and evaluated yielding the same performance of the previous case. © 2003 by ***, ***, ***, ***, ***.

关键词： Flight simulators

来源：评论

学校读者我要写书评

暂无评论

Satellite simulator for integrated simulation of virtual spacecraft bus and communications payload

Satellite simulator for integrated simulation of virtual spa...

引用

aiaa modeling and simulation technologies conference and exhibit 2003

作者： Kang, Ja-Young Department of Aeronautical Science and Flight Operation Hankuk Aviation University Goyang Korea Republic of

ISBN: (纸本)9781624100918

A communications payload has been developed and its flight model will be launched with a Korean Experimental Satellite. For the purpose of a functional test and verification of the payload, a spacecraft simulator has also been developed. This simulator is a real-time, hardware-in-the-loop system, which runs under a PC-based simulation environment using a Windows operating system. The simulator provides a low-cost tool to test and verify the communication payload as well as the integrated simulation of a hardware payload and a virtual spacecraft. We assumed that the spacecraft platform for the simulator is a geostationary communications satellite that uses a momentum-biased three-axis stabilization control technique. The payload is combined with the simulator via power, command, and a telemetry module of electrical ground support equipment. The operator's commands to the satellite are transferred to the payload or bus subsystem models via the real-time kernel of the simulator. In this paper, the design architecture and operation functions of the system will be discussed in detail. © 2003 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.

关键词： Satellite simulators

来源：评论

学校读者我要写书评

暂无评论

Using the simona research simulator for human-machine interaction research

Using the simona research simulator for human-machine intera...

引用

aiaa modeling and simulation technologies conference and exhibit 2003

作者： Stroosma, Olaf van Paassen, René Mulder, Max International Research Institute for Simulation Motion and Navigation Delft University of Technology Delft Netherlands Control and Simulation Division Delft University of Technology Delft Netherlands

ISBN: (纸本)9781624100918

The Delft University of Technology has developed a 6 degree-of-freedom flight simulator, the SIMONA Research Simulator (SRS). The design incorporates several advanced technologies, such as light-weight construction, high performance motion drive algorithms and a flexible, PC-based computer infrastructure. The simulator serves as a testbed for new technologies and as a tool for Human-Machine Interaction (HMI) research. Key components of the simulator that allow high quality Human-Machine Interaction research to be performed, are described. To ensure a sufficient level of accessibility for students and researchers, the software architecture of the SRS uses the Delft University Environment for Communication and Activation (DUECA), a middleware layer that shields the user from the complexities of the communication between PCs and the real-time scheduling of the different simulation modules. Through the use of DUECA, experiments are also easily portable between development workstations and different simulator environments. The concepts behind DUECA and its use in the research environment of SIMONA are discussed. Several research projects with the Faculty of Aerospace Engineering of the Delft University of Technology have been performed successfully using DUECA, on simulators of different fidelity, from standalone PCs, to a fixed base mockup and the SRS. © 2003 by Delft University of Technology. Published by the American Institute of Aeronautics and Astronautics, Inc.

关键词： Flight simulators

来源：评论

学校读者我要写书评

暂无评论

Rapid prototyping of an aircraft model in an object-oriented simulation

Rapid prototyping of an aircraft model in an object-oriented...

引用

aiaa modeling and simulation technologies conference and exhibit 2003

作者： Sean Kenney, P. Systems Development Branch NASA Langley Research Center Mail Stop 125B Hampton VA 23681 United States

ISBN: (纸本)9781624100918

A team was created to participate in the Mars Scout Opportunity. Trade studies determined that an aircraft provided the best opportunity to complete the science objectives of the team. A high fidelity six degree of freedom flight simulation was required to provide credible evidence that the aircraft design fulfilled mission objectives and to support the aircraft design process by providing performance evaluations. The team created the simulation using the Langley Standard Real-Time simulation in C++ (LaSRS++) application framework. A rapid prototyping approach was necessary because the team had only three months to both develop the aircraft simulation model and evaluate aircraft performance as the design and mission parameters matured. The design of LaSRS++ enabled rapid-prototyping in several ways. First, the framework allowed component models to be designed, implemented, unit-tested, and integrated quickly. Next, the framework provides a highly reusable infrastructure that allowed developers to maximize code reuse while concentrating on aircraft and mission specific features. Finally, the framework reduces risk by providing reusable components that allow developers to build a quality product with a compressed testing cycle that relies heavily on unit testing of new components.

关键词： Rapid prototyping

来源：评论

学校读者我要写书评

暂无评论

Futureflight central: A revolutionary air traffic control tower simulation facility

Futureflight central: A revolutionary air traffic control to...

引用

aiaa modeling and simulation technologies conference and exhibit 2003

作者： Dorighi, Nancy S. Sullivan, Barry T. NASA Ames Research Center Moffett Field CA United States

ISBN: (纸本)9781624100918

A new air traffic control tower research facility dedicated to countering potential air and runway traffic problems at commercial airports is advancing the stateof-the-art in aviation research at the National Aeronautics and Space Administration (NASA) Ames Research Center. FutureFlight Central (FFC), is a unique real-time simulator designed to safely study new technologies, airport design changes or redesigns, and procedural changes in a virtual reality setting. The facility consists of a full-scale control tower, which depicts a 360-degree view of the airport under various weather conditions and times of day. Actual air traffic controllers operate the tower and communicate with pilots, ramp controllers and vehicle operators. "Humans-in-the-loop" provide a key distinction between conventional fast time simulation and what NASA has created in FFC. Human factors such as situational awareness, reaction time, visual perception and oral communication validate new designs and tools at a significantly higher level of accuracy and confidence. Recent integration of the tower with fullmission flight simulation allows assessment of airport changes from both the controller and pilot perspectives. With this new capability, technology developers, airport planners, and airline representatives are able to make more informed decisions. This paper describes the capabilities of FutureFlight Central, provides examples of typical projects, and addresses future applications.

关键词： NASA

来源：评论

学校读者我要写书评

暂无评论

Hydra: High-speed simulation architecture for precision spacecraft formation simulation

Hydra: High-speed simulation architecture for precision spac...

引用

aiaa modeling and simulation technologies conference and exhibit 2003

作者： Martin, Bryan J. Sohlt, Garett A. Jet Propulsion Laboratory Pasadena CA United States

ISBN: (纸本)9781624100918

Hydra- the Hierarchical Distributed Reconflgurable Architecture - is a scalable simulation architecture that provides flexibility and ease-of-use which take advantage of modern computation and communication hardware. It also provides the ability to implement distributed- or workstation -based simulations and high-fidelity real-time simulation from a common core. Originally designed to serve as a research platform for examining fundamental challenges in formation flying simulation for future space missions, it is also finding use in other missions and applications, all of which can take advantage of the underlying Object-Oriented structure to easily produce distributed simulations. Hydra automates the process of connecting disparate simulation components (Hydra Clients) through a client-server architecture that uses high-level descriptions of data associated with each client to find and forge desirable connections (Hydra Services) at run time. Services communicate through the use of Connectors, which abstract messaging to provide single-interface access to any desired communication protocol, such as from shared-memory message passing or TCP/IP to ACE1 and CORBA.2 Hydra shares many features with the HLA,3 although providing more flexibility in connectivity services and behavior overriding. © 2003 by the American Institute of Aeronautics and Astronautics, Inc.

关键词： Common object request broker architecture (CORBA)

来源：评论

学校读者我要写书评

暂无评论

Characteristics and applications of the new high level architecture - HLA to parallel or distributed simulation and control of aerospace vehicles

Characteristics and applications of the new high level archi...

引用

aiaa modeling and simulation technologies conference and exhibit 2003

作者： Da Cunha Trivelato, Gilberto de Oliveira e Souza, Marcelo Lopes EMBRAER - Empresa Brasileira de Aeronáutica S. A P.O. Box 8050 12227-901 - S. José dos Campos - SP Brazil INPE - National Institute for Space Research DMC - Division of Space Mechanics and Control Av. dos Astronautas 1758 12227-010 - S. José dos Campos - SP Brazil

ISBN: (纸本)9781624100918

In this work we discuss the characteristics and applications of the New High Level Architecture-HLA to parallel or distributed simulation and control of aerospace vehicles. HLA is a new standard that is being developed since 1996 to replace previous standards as the Distributed Interactive simulation -DIS standard in the tasks of interconnecting the main elements of parallel or distributed simulation and control through a common Run Time Infrastructure-RTI. HLA is being developed under the technical guidance and administrative leadership of the Defense modeling and simulation Office - DMSO of the Department of Defense - DOD of USA. Since 1998 DOD imposed successive (no pay-1998, no play-1999) deadlines to the defense industry for ending the use of previous standards and beginning the use of HLA. Since then and due to that, its adoption is growing steadily, and its versions matured rapidly to the point that it became the IEEE 1516 standard for modeling and simulation in 2000. This is the version whose characteristics (Interoperability, Reuse, Connectivity, Open Standard, Run Time Infrastructure, Maturity, Adherence to legacy projects and to object oriented projects, etc.) will be discussed in this work, specially for applications to parallel or distributed simulation and control of aerospace vehicles. © 2003 by Gilberto C. Trivelato & Marcelo L. O. Souza.

关键词： Vehicles

来源：评论

学校读者我要写书评

暂无评论

Agent-based support for distributed air/ground traffic management simulation research

Agent-based support for distributed air/ground traffic manag...

引用

aiaa modeling and simulation technologies conference and exhibit 2003

作者： Callantine, Todd J. Prevôt, Thomas Battiste, Vernol Johnson, Walter W. San Jose State University NASA Ames Research Center Moffett Field CA 94035-1000 United States

ISBN: (纸本)9781624100918

NASA researchers are extending a large-scale distributed simulation to assess the feasibility, benefits, and scalability of Distributed Air/Ground Traffic Management (DAG-TM) concepts. This paper describes applications of software agents to support these efforts. This paper identifies applications ranging from assistants to replacements for human confederate participants and support personnel. The applications span air traffic control positions, flight simulators, pseudo-aircraft control stations, and simulation support functions. The paper first provides an overview of the DAG-TM simulation, including the Multi Aircraft Control System (MACS), and describes the responsibilities of various participants. It then discusses agent applications that address problems and leverage capabilities demonstrated in previous research. Of particular interest are agents that can control air traffic and pilot aircraft, implemented within the MACS framework. Agents provide a means for focusing required subject training, reducing variability and problems attributable to human confederates, supporting partially staffed and part-task studies within the full simulation environment, and enabling fast-time simulations to investigate DAG-TM concept scalability. The paper concludes with a discussion that emphasizes the importance of interplay between complementary human-in-the-loop and agent-based simulations. This research constitutes one facet of the Distributed Air/Ground Traffic Management element of the NASA Aviation System Capacity Program Advanced Air Transportation technologies project.

关键词： Air traffic control

来源：评论

学校读者我要写书评

暂无评论

A flight trajectory model for a pc-based airspace analysis tool

A flight trajectory model for a pc-based airspace analysis t...

引用

aiaa modeling and simulation technologies conference and exhibit 2003

作者： Mayer, Ralf H. McLean VA 22102 United States

ISBN: (纸本)9781624100918

This paper documents a method for rapid generation of aircraft flight trajectories. Rapid generation of flight trajectories is important for simulation models of air traffic that involve large numbers of aircraft, especially if complex interdependencies exist between flights and short simulation run times are required. Among the many aircraft trajectory models that have been developed, one generally observes a tradeoff between modeling detail provided by the model and its computational speed. Models that provide detailed trajectories typically require simulation run times on the order of one second per trajectory. Faster models often trade modeling detail for greater simulation speed. The model presented here was developed for applications that require simulation speeds on the order of one thousand trajectories per second and modeling detail to simulate typical flight operations in airspace close to major airports known as Terminal Radar Approach Control (TRACON) airspace. The computational speed of the model results from a discrete event simulation approach. It generates continuous speed and altitude profiles based on a small set of 31 trajectory parameters that are defined for each aircraft type based on aircraft performance data. The model provides detailed flight trajectories by synchronizing the discrete events that define model trajectories with significant events of typical flight operations and methodically adjusting the size of variable simulation time steps. The time steps, chosen in accordance with common piloting procedures and flight events, are categorized in ten flight phases. This paper introduces the concept of flight phases to group flight events and their associated trajectory parameters and presents a discrete-event flight trajectory model that is based on aircraft performance and centered on piloting procedures. © 2003 by The Mitre Corporation.

关键词： Discrete event simulation

来源：评论

学校读者我要写书评

暂无评论

Automated modeling and simulation using the bond graph method for the aerospace industry

Automated modeling and simulation using the bond graph metho...

引用

aiaa modeling and simulation technologies conference and exhibit 2003

作者： Granda, Jose J. Montgomery, Raymond C. Department of Mechanical Engineering California State University Sacramento Sacramento 95819 CA United States Dynamics and Control Branch NASA Langley Research Center Hampton VA 23681 United States

ISBN: (纸本)9781624100918

Bond graph modeling was originally developed in the late 1950s by the late Prof. Henry M. Paynter of M.I.T. Prof. Paynter acted well before his time as the main advantage of his creation, other than the modeling insight that it provides and the ability of effectively dealing with Mechatronics, came into fruition only with the recent advent of modern computer technology and the tools derived as a result of it, including symbolic manipulation, MATLAB, and SIMULINK and the Computer Aided modeling Program (CAMPG). Thus, only recently have these tools been available allowing one to fully utilize the advantages that the bond graph method has to offer. The purpose of this paper is to help fill the knowledge void concerning its use of bond graphs in the aerospace industry. The paper first presents simple examples to serve as a tutorial on bond graphs for those not familiar with the technique. The reader is given the basic understanding needed to appreciate the applications that follow. After that, several aerospace applications are developed such as modeling of an arresting system for aircraft carrier landings, suspension models used for landing gears and multibody dynamics. The paper presents also an update on NASA's progress in modeling the International Space Station (ISS) using bond graph techniques, and an advanced actuation system utilizing shape memory alloys. The later covers the Mechatronics advantages of the bond graph method, applications that simultaneously involves mechanical, hydraulic, thermal, and electrical subsystem modeling.

关键词： Aerospace industry

来源：评论

学校读者我要写书评

暂无评论

没有更多数据了...

全选清除本页清除全部题录导出标记到“检索档案”

共29页 << < 7 8 9 10 11 12 13 14 15 16 > >>

检索报告对象比较合并检索0

隐藏清空

合并搜索

回到顶部

执行限定条件

内容：

评分：

请选择保存的检索档案：

请选择收藏分类：

订阅名称：

通借通还

温馨提示：

图书名称：

借书校区：

取书校区：

手机号码：

邮箱地址：

一卡通帐号：

电话和邮箱必须正确填写，我们会与您联系确认。

联系人：

所在院系：

联系邮箱：

联系电话：

内蒙古自治区呼和浩特市赛罕区大学西街235号邮编: 010021

建议与咨询 留下您的常用邮箱和电话号码，以便我们向您反馈解决方案和替代方法

时间限定

文献类型

馆藏选择

核心期刊

语言

文献类型

帮助

文字说明：

检索规则说明：

检索范例：

分类表

所选分类

限定检索结果

文献类型

馆藏范围

日期分布

学科分类号

主题

机构

作者

语言

请选择保存的检索档案： 新增检索档案 确定 取消

请选择收藏分类： 新增自定义分类 确定 取消

通借通还

建议与咨询留下您的常用邮箱和电话号码，以便我们向您反馈解决方案和替代方法

请选择保存的检索档案：

请选择收藏分类：