9th IEEE/AIAA/NASA Conference on Digital Avionics Systems最新文献_第7页

A military avionics 32-bit advance modular processor system 一种军用航空电子32位先进模块化处理器系统

9th IEEE/AIAA/NASA Conference on Digital Avionics Systems Pub Date : 1990-10-15 DOI: 10.1109/DASC.1990.111333

D. R. Witzel

引用次数: 0

Advanced Information Processing System (AIPS)-based fault tolerant avionics architecture for launch vehicles 基于先进信息处理系统(AIPS)的运载火箭航空电子容错体系结构

9th IEEE/AIAA/NASA Conference on Digital Avionics Systems Pub Date : 1990-10-15 DOI: 10.1109/DASC.1990.111274

J. Lala, R. Harper, K. R. Jaskowiak, G. Rosch, L. Alger, A. Schor

{"title":"Advanced Information Processing System (AIPS)-based fault tolerant avionics architecture for launch vehicles","authors":"J. Lala, R. Harper, K. R. Jaskowiak, G. Rosch, L. Alger, A. Schor","doi":"10.1109/DASC.1990.111274","DOIUrl":"https://doi.org/10.1109/DASC.1990.111274","url":null,"abstract":"An avionics architecture for the advanced launch system (ALS) that uses validated hardware and software building blocks developed under the advanced information processing system program is presented. The AIPS for ALS architecture is preliminary, and reliability requirements can be met by the AIPS hardware and software building blocks that are built using the state-of-the-art technology available in the 1992-3 time frame. The level of detail in the architecture definition reflects the level of detail available in the ALS requirements. As the avionics requirements are refined, the architecture can also be refined and defined in greater detail with the help of analysis and simulation tools. A useful methodology is demonstrated for investigating the impact of the avionics suite to the recurring cost of the ALS. It is shown that allowing the vehicle to launch with selected detected failures can potentially reduce the recurring launch costs. A comparative analysis shows that validated fault-tolerant avionics built out of Class B parts can result in lower life-cycle-cost in comparison to simplex avionics built out of Class S parts or other redundant architectures.<<ETX>>","PeriodicalId":141205,"journal":{"name":"9th IEEE/AIAA/NASA Conference on Digital Avionics Systems","volume":"91 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1990-10-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129503399","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: 19

Integrated toolset for high-integrity system verification and validation support (avionics) 用于高完整性系统验证和验证支持的集成工具集(航空电子)

9th IEEE/AIAA/NASA Conference on Digital Avionics Systems Pub Date : 1990-10-15 DOI: 10.1109/DASC.1990.111298

R.P. Cabos

引用次数: 0

Artificial intelligence programming in Ada Ada中的人工智能编程

9th IEEE/AIAA/NASA Conference on Digital Avionics Systems Pub Date : 1990-10-15 DOI: 10.1109/DASC.1990.111279

K.R. Leeper

引用次数: 1

A fault tolerant fly by wire system for maintenance free applications 一个容错飞线系统的免维护应用程序

9th IEEE/AIAA/NASA Conference on Digital Avionics Systems Pub Date : 1990-10-15 DOI: 10.1109/DASC.1990.111255

R. Dennis, A. Hills

{"title":"A fault tolerant fly by wire system for maintenance free applications","authors":"R. Dennis, A. Hills","doi":"10.1109/DASC.1990.111255","DOIUrl":"https://doi.org/10.1109/DASC.1990.111255","url":null,"abstract":"The authors describe a triplex primary flight computer system based on a reconfigurable architecture with extensive use of application specific integrated circuits (ASICs). The system comprises fault-tolerant fly-by-wire (FBW) computers which are triplex dissimilar in both software and hardware. These command actuator control electronics (ACE) units via DATAC (ARINC 629) data buses. The FBW computers form the core of the full-authority FBW system and perform all the computational commands for the pitch, roll, and yaw surface actuation systems. The authors review the architectural design issues in terms of integrity requirements and fault tolerance, leading to a design which not only meets civil safety requirements but also has ultra-high-reliability, offering little or no maintenance action. The FBW computer architecture is based on dividing the basic path into three subfunctional elements. Each of these elements is then replicated to provide fault tolerance. The internal element redundancy management function is performed both in hardware and software, and it is able to detect and isolate faulty elements and perform the necessary reconfiguration. The current expectation for system reliability gives an expected time to 95% probability of dispatch of 38100 operating hours and has a predicted MTBMA of 92700 operating hours per shipset.<<ETX>>","PeriodicalId":141205,"journal":{"name":"9th IEEE/AIAA/NASA Conference on Digital Avionics Systems","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1990-10-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129140383","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: 9

Content addressable memory for electronic warfare sensor signature identification 用于电子战传感器签名识别的内容可寻址存储器

9th IEEE/AIAA/NASA Conference on Digital Avionics Systems Pub Date : 1990-10-15 DOI: 10.1109/DASC.1990.111284

L. P. Butler, J.E. Meisenbacher

引用次数: 0

Automated code generation for application engineers (avionics) 为应用工程师(航空电子)自动生成代码

9th IEEE/AIAA/NASA Conference on Digital Avionics Systems Pub Date : 1990-10-15 DOI: 10.1109/DASC.1990.111358

J.J. Turkovich

引用次数: 4

Validation of the F-18 high alpha research vehicle flight control and avionics systems modifications 验证F-18高α研究载具飞行控制和航空电子系统修改

9th IEEE/AIAA/NASA Conference on Digital Avionics Systems Pub Date : 1990-10-15 DOI: 10.1109/DASC.1990.111254

V. Chacon, J. Pahle, V.A. Regenie

{"title":"Validation of the F-18 high alpha research vehicle flight control and avionics systems modifications","authors":"V. Chacon, J. Pahle, V.A. Regenie","doi":"10.1109/DASC.1990.111254","DOIUrl":"https://doi.org/10.1109/DASC.1990.111254","url":null,"abstract":"The authors discuss the tests, tools, and techniques used for the validation of the F-18 high alpha research vehicle (HARV) turning vane control system (TVCS), and document the problems and their solutions. The HARV system modification to add a research flight control system (RFCS) and TVCS included the integration of avionics, engine parameters, and external inputs into the flight control system. This integration introduced flexible experimental components into the system. The validation of the HARV system modification included many aspects. The system design included the capability to extract internal parameters from the control system. The interface between the RFCS and the basic F-18 system contained checks and balances to ensure that the safety of the total system was not compromised by unforeseen circumstances. The testing addressed critical issues to ensure the backup system was not compromised by the addition of the experimental systems. The integrated test facility systems were used to automate repetitive tests and collect large amounts of data, and allowed the test team to concentrate on interpreting test results rather than the test system. The test team encountered problems with the system under test with the inability to sort through the information in an efficient manner, to maintain communications over large distances, and to obtain desired results in a timely manner.<<ETX>>","PeriodicalId":141205,"journal":{"name":"9th IEEE/AIAA/NASA Conference on Digital Avionics Systems","volume":"86 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1990-10-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126948876","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: 8

A threshold redundancy management algorithm for skewed sensor arrays 偏斜传感器阵列的阈值冗余管理算法

9th IEEE/AIAA/NASA Conference on Digital Avionics Systems Pub Date : 1990-10-15 DOI: 10.1109/DASC.1990.111275

F. E. DeAngelis

引用次数: 7

The Pegasus avionics system design 飞马航空电子系统设计

9th IEEE/AIAA/NASA Conference on Digital Avionics Systems Pub Date : 1990-10-15 DOI: 10.1109/DASC.1990.111309

D.A. Steffy

引用次数: 1