1996 IEEE Aerospace Applications Conference. Proceedings最新文献_第3页

Aerospace applications of optical sensing with lidar 激光雷达光学传感的航空航天应用

1996 IEEE Aerospace Applications Conference. Proceedings Pub Date : 1996-02-03 DOI: 10.1109/AERO.1996.495968

S. Beck, J. Gelbwachs, D. Hinkley, D. Warren, J. Wessel

引用次数: 4

SatTrack (V4.0)-a real-time satellite tracking and orbit prediction program SatTrack (V4.0)-实时卫星跟踪和轨道预测程序

1996 IEEE Aerospace Applications Conference. Proceedings Pub Date : 1996-02-03 DOI: 10.1109/AERO.1996.499660

Manfred Bester

引用次数: 2

A microelectromechanical quartz rotational rate sensor for inertial applications 一种用于惯性应用的微机电石英转速传感器

1996 IEEE Aerospace Applications Conference. Proceedings Pub Date : 1996-02-03 DOI: 10.1109/AERO.1996.495986

A. Madni, L. A. Wan, S. Hammons

引用次数: 28

Space technology transition using hardware in the loop simulation 空间技术转型利用硬件在环仿真

1996 IEEE Aerospace Applications Conference. Proceedings Pub Date : 1996-02-03 DOI: 10.1109/AERO.1996.495985

J. Leitner

{"title":"Space technology transition using hardware in the loop simulation","authors":"J. Leitner","doi":"10.1109/AERO.1996.495985","DOIUrl":"https://doi.org/10.1109/AERO.1996.495985","url":null,"abstract":"This paper treats the development of a laboratory within the USAF Phillips Lab for the purpose of integrating component technologies and demonstrating spacecraft subsystem/payload level capabilities. The lab will facilitate the transition of technologies to flight. The infrastructure will be such that virtually any type of spacecraft payload or subsystem can be brought in, as long as the technologies are mature. The emphasis is placed upon the hardware in the loop (HIL) simulation evaluation. End to end HIL simulation has several benefits within the Phillips Lab, including (1) bringing forth spacecraft integration problems before spending millions of dollars to put a system into space, (2) exploring scenarios for in-flight anomalies and hardware and software failures, (3) showing the utility of component technologies and subsystems to the warfighter, (4) evaluating various potential mission concepts, (5) selling programs to upper management, (6) training of operators and educating lab personnel in how theater operations are performed with respect to obtaining data from space, Based on monetary constraints, the lab must leverage off of existing hardware in the loop facilities, such as Wright Lab's Kinetic Kill Vehicle HIL facility (KHILS), JPL's Flight System Testbed (FST), Arnolds Engineering Development Center (AEDC), etc., in terms of networking in, mimicking equipment, and utilizing lessons learned. The cost for setting up the HIL facility will be further reduced by building the lab based on requirements for the individual projects coming in, rather than up front construction of a HIL laboratory.","PeriodicalId":262646,"journal":{"name":"1996 IEEE Aerospace Applications Conference. Proceedings","volume":"2 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1996-02-03","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130261274","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 22

Process definition for rapid architecture development 快速架构开发的过程定义

1996 IEEE Aerospace Applications Conference. Proceedings Pub Date : 1996-02-03 DOI: 10.1109/AERO.1996.496072

A. Shetler

{"title":"Process definition for rapid architecture development","authors":"A. Shetler","doi":"10.1109/AERO.1996.496072","DOIUrl":"https://doi.org/10.1109/AERO.1996.496072","url":null,"abstract":"A rapid architecture development process was used to design an architecture concept that provided system requirements for the command, control, communications and intelligence (C3I) system component of a major weapon platform. This paper describes the architecture process, including the activities and associated tasks, to develop the architecture concept. The architecture concept defined the system component's life cycle framework. The architecture process is based on TRW's system and software engineering process assets. The process description includes a discussion of the engineering activities and the four principal system engineering processes used to direct the work effort: (1) architecture framework, which established the scope of the architecture; (2) requirements management, which established the boundaries for the architecture; (3) modeling and simulation, which established performance requirements and drove the architecture preliminary design; and (4) analyses, which provided overall substantiation for the engineering architecture effort. The process guided the rapid development of the C3I system architecture concept; the work was part of a concurrent engineering effort.","PeriodicalId":262646,"journal":{"name":"1996 IEEE Aerospace Applications Conference. Proceedings","volume":"14 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1996-02-03","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"121476869","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 2

3-D electronic interconnect packaging 三维电子互连封装

1996 IEEE Aerospace Applications Conference. Proceedings Pub Date : 1996-02-03 DOI: 10.1109/AERO.1996.495896

K. Sienski, R. Eden, D. Schaefer

引用次数: 30

Geometric feature extraction using the chord transformation 利用弦变换提取几何特征

1996 IEEE Aerospace Applications Conference. Proceedings Pub Date : 1996-02-03 DOI: 10.1109/AERO.1996.499675

J. Selvage, D. Chenoweth, V. E. Gold

引用次数: 1

An airborne ground penetrating radar system 一种机载探地雷达系统

1996 IEEE Aerospace Applications Conference. Proceedings Pub Date : 1996-02-03 DOI: 10.1109/AERO.1996.495881

W. Gregorwich

引用次数: 4

System fault protection design for the Cassini spacecraft 卡西尼号航天器系统故障保护设计

1996 IEEE Aerospace Applications Conference. Proceedings Pub Date : 1996-02-03 DOI: 10.1109/AERO.1996.495890

John P. Slonslu

引用次数: 6

Simulation of active circuit survivability 有源电路生存性仿真

1996 IEEE Aerospace Applications Conference. Proceedings Pub Date : 1996-02-03 DOI: 10.1109/AERO.1996.495900

L. Wiederspahn, K. Chung, J. Canyon

引用次数: 0