Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings最新文献

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Performing the Galileo mission using the S-band low-gain antenna 使用s波段低增益天线执行伽利略任务
Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings Pub Date : 1994-02-05 DOI: 10.1109/AERO.1994.291197
J. Marr
{"title":"Performing the Galileo mission using the S-band low-gain antenna","authors":"J. Marr","doi":"10.1109/AERO.1994.291197","DOIUrl":"https://doi.org/10.1109/AERO.1994.291197","url":null,"abstract":"Following the failure of Galileo's X-band high-gain antenna to deploy in April 1991, an alternate approach which utilizes the spacecraft's S-band low-gain antenna has been conceived and is in development. This approach will enable the accomplishment of at least 70 percent of Galileo's original scientific objectives. Implementation is to be accomplished in two steps, called Phase 1 and Phase 2, each of which requires changes to both the Galileo spacecraft software and to the supporting ground systems. This paper presents an overview of the Galileo mission and describes in some detail the changes required to implement both phases and which are under development by the worldwide Galileo team.<<ETX>>","PeriodicalId":223269,"journal":{"name":"Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings","volume":"131 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1994-02-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"115829965","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: 6
Carrier false lock performance for TDRS TT&C transponder TDRS TT&C应答器的载波假锁性能
Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings Pub Date : 1994-02-05 DOI: 10.1109/AERO.1994.291184
C. Tsang
{"title":"Carrier false lock performance for TDRS TT&C transponder","authors":"C. Tsang","doi":"10.1109/AERO.1994.291184","DOIUrl":"https://doi.org/10.1109/AERO.1994.291184","url":null,"abstract":"In this paper the mechanism of carrier false lock phenomenon of a design of TDRS TT&C transponder is analyzed in details. It is found that the carrier false lock is due to the excessive time delays in the filters and other electronic components in the long tracking loop. The stability of the AGC and the command lock out issues of the same transponder are also addressed. Suggestions on the fixes are also provided.<<ETX>>","PeriodicalId":223269,"journal":{"name":"Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings","volume":"39 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1994-02-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"121061342","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: 3
An electronically scanned dual-polarized antenna for tracking multiple targets simultaneously 一种电子扫描双极化天线,用于同时跟踪多个目标
Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings Pub Date : 1994-02-05 DOI: 10.1109/AERO.1994.291192
W. Gregorwich, R. Ward, R.A. Hall
{"title":"An electronically scanned dual-polarized antenna for tracking multiple targets simultaneously","authors":"W. Gregorwich, R. Ward, R.A. Hall","doi":"10.1109/AERO.1994.291192","DOIUrl":"https://doi.org/10.1109/AERO.1994.291192","url":null,"abstract":"A compact electronically scanned array is described that provides full hemispherical coverage with both left hand (LH) and right hand circular polarization (RHCP). By means of unique surface acoustic wave devices and variable power combiners, the microprocessor controlled, autonomous antenna tracked and received telemetry data from four submarine launched Trident missiles. Almost identical performance has been measured for both LHCP and RHCP from the same helical antenna.<<ETX>>","PeriodicalId":223269,"journal":{"name":"Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings","volume":"8 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1994-02-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"134591923","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: 4
Zone plate reflector antennas for applications in space 空间用带板反射天线
Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings Pub Date : 1994-02-05 DOI: 10.1109/AERO.1994.291189
H.A. Malliot
{"title":"Zone plate reflector antennas for applications in space","authors":"H.A. Malliot","doi":"10.1109/AERO.1994.291189","DOIUrl":"https://doi.org/10.1109/AERO.1994.291189","url":null,"abstract":"The zone plate (ZP) reflector antenna is presented as a low cost, low weight alternative to parabolic reflector and array antennas on satellites and interplanetary spacecraft when antennas with high gain and low sidelobes are required. The reflector efficiency of a zone plate antenna with four phase segments in each Bone is 95 percent. The directional patterns of zone plate antennas were computed by recursive integration of the circular aperture Fresnel integral. Computed antenna patterns are similar to the pattern of a uniformly illuminated parabolic reflector. The ZP reflector has 4 to 5 percent larger beamwidth than the same diameter parabolic reflector, and the first sidelobe level approaches /spl minus/17.7 dB as the number of zones increases. Peak sidelobe levels decrease monotonically. The beamwidth increases and peak sidelobe levels decrease as edge illumination decreases. Chromatic aberration limits the instantaneous bandwidth of a zone plate antenna, but the antenna can be tuned over broad frequency bands by moving the feed position. Aberration limited scan angles are larger than obtainable with parabolic reflectors but, for a given scan angle, the maximum frequency for aberration free beam forming reduces with plate diameter and increases with the F-number. Achievement of large scan angles at K-band and higher frequencies requires corrective optics. Zone plate antennas can be used in a variety of applications where low cost, low weight, multiple beam or scanning of a narrow beam over a large angular field are required.<<ETX>>","PeriodicalId":223269,"journal":{"name":"Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1994-02-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129452758","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
Reactive antenna matching when using integrated optical modulators 使用集成光调制器时的无功天线匹配
Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings Pub Date : 1994-02-05 DOI: 10.1109/AERO.1994.291186
M. Grace, M. VanBlaricum, T. Larry, P. Stieber
{"title":"Reactive antenna matching when using integrated optical modulators","authors":"M. Grace, M. VanBlaricum, T. Larry, P. Stieber","doi":"10.1109/AERO.1994.291186","DOIUrl":"https://doi.org/10.1109/AERO.1994.291186","url":null,"abstract":"The use of externally modulated fiber optic links for antenna remoting provides new opportunities for high performance, but requires no electrical power at the remote end. For those applications where wide instantaneous bandwidth is not essential, reactive matching can provide a very low link noise figure. At lower frequencies (typically <50O MHz), using reactive tuning elements in conjunction with a transformer can theoretically yield a noise figure below the 3 dB limit for passive systems. The externally modulated system in this case is not a truly passive system but can be thought of as an optically-driven RF amplifier.<<ETX>>","PeriodicalId":223269,"journal":{"name":"Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings","volume":"12 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1994-02-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130005895","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: 1
Microwave CLO sounder 微波CLO测深仪
Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings Pub Date : 1994-02-05 DOI: 10.1109/AERO.1994.291178
H. Malliot
{"title":"Microwave CLO sounder","authors":"H. Malliot","doi":"10.1109/AERO.1994.291178","DOIUrl":"https://doi.org/10.1109/AERO.1994.291178","url":null,"abstract":"Describes the design of a satellite borne microwave radiometer operating at the frequency of 204.352 GHz for sounding the abundance of stratospheric chlorine oxide (CLO). The CLO sounder is assumed to be at an altitude of 600 km and observes the atmosphere at tangential range of 2780 km at 20 km altitude. The altitude range from 15 km to 45 km is observed in eleven tracks with center-center spacing of 2.73 km and widths of 3.1 km. An innovative antenna design uses a 1.7 m diameter offset feed zone plate reflector and an assembly of feed horns to provide eleven simultaneous beams in the elevation plane with beam-beam angular separations of 0.056 degree and beamwidths of 0.064 degree. Secondary and a tertiary reflectors direct the beams onto an array of feed horns. The secondary reflector provides compensation for aberrations due to the off-axis geometry. The tertiary reflector switches the observed source among soundings and cold sky and hot load calibrations. A low risk radiometer design uses direct down conversion by two stage mixing to convert the 204.352 GHz signal to a 510 MHz band centered at 600 MHz. The 600 MHz IF signal is input to a filter bank which produces outputs in 15 channels with bandwidths from 2 to 128 MHz. With two second integration, the radiometer sensitivity is 0.35 K with 2 MHz bandwidth and 0.04 K with 128 MHz bandwidth. Calibration is provided by periodic hot load and cold sky views.<<ETX>>","PeriodicalId":223269,"journal":{"name":"Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1994-02-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130785912","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: 1
A telemetering educational graduate program: the aerospace applications test and evaluation dimension 遥测教育研究生课程:航空航天应用测试与评估维度
Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings Pub Date : 1994-02-05 DOI: 10.1109/AERO.1994.291205
F. Carden
{"title":"A telemetering educational graduate program: the aerospace applications test and evaluation dimension","authors":"F. Carden","doi":"10.1109/AERO.1994.291205","DOIUrl":"https://doi.org/10.1109/AERO.1994.291205","url":null,"abstract":"A Telemetering Center of Excellence, a Chair of Telemetering, and an educational program in telemetering systems engineering leading to a Masters Degree in Electrical Engineering have been established at New Mexico State University in cooperation with the International Foundation for Telemetering, the supporting industry, the government ranges, and NASA. Although one of the primary goals of the program is to graduate MS students who understand the concept of \"end-to-end\" telemetering system design for test and evaluation, another goal is to incorporate the latest aerospace applications with the attendant test and evaluation technology used in the development stage into the educational process. This paper covers two aspects of the telemetering educational program: (1) specific technological developments which have a substantial impact in the teaching program and (2) the curriculum.<<ETX>>","PeriodicalId":223269,"journal":{"name":"Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings","volume":"30 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1994-02-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116743462","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: 0
An overview of object-oriented design and C++ 面向对象设计和c++的概述
Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings Pub Date : 1994-02-05 DOI: 10.1109/AERO.1994.291202
R. R. Seban
{"title":"An overview of object-oriented design and C++","authors":"R. R. Seban","doi":"10.1109/AERO.1994.291202","DOIUrl":"https://doi.org/10.1109/AERO.1994.291202","url":null,"abstract":"The object-oriented software development methodology is rapidly replacing the structure-oriented development methodology. The object-oriented software design stage of the software development cycle, informally, consists of partitioning of the problem into a set of communicating entities called objects. Each object is an instance of a framework called a class. Each class defines a structure consisting of a collection of data and a set of functions (called methods) permitted to operate on the class data. The object-oriented language C++ (based on the highly popular \"C\" language) has become the de-facto standard for the object-oriented software programming. In this paper we present an overview of the object-oriented design and object-oriented programming stages of the software development cycle. We briefly discuss the object-oriented software development cycle to provide the context for the design and programming stages. We discuss the design and implementation of a class, and the development of a software project utilizing the object-oriented principles.<<ETX>>","PeriodicalId":223269,"journal":{"name":"Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings","volume":"173 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1994-02-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132105876","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: 7
Sneak circuit path within a DPDT relay DPDT继电器内的偷偷电路路径
Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings Pub Date : 1994-02-05 DOI: 10.1109/AERO.1994.291182
M. Rosenthal, L. Mallette, K. Ishikawa, J. Varney
{"title":"Sneak circuit path within a DPDT relay","authors":"M. Rosenthal, L. Mallette, K. Ishikawa, J. Varney","doi":"10.1109/AERO.1994.291182","DOIUrl":"https://doi.org/10.1109/AERO.1994.291182","url":null,"abstract":"A failed resistor in an electronic circuit was found to have been subjected to an overvoltage condition. One side of the resistor was connected to a dual-coil DPDT latching relay, and the other side to ground. The cause of this failure was found to be due to a threefold problem: 1. A test set that, when powered on, would send simultaneous commands to both relay coils. 2. A sneak path through the relay when both relay coils were simultaneously energized. 3. A design that did not consider this sneak path.<<ETX>>","PeriodicalId":223269,"journal":{"name":"Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings","volume":"81 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1994-02-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"132588953","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
The Benefield Anechoic Facility (BAF) threat generation system 贝尼菲尔德消声设备(BAF)威胁生成系统
Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings Pub Date : 1994-02-05 DOI: 10.1109/AERO.1994.291198
R. Smith, R. Taylor
{"title":"The Benefield Anechoic Facility (BAF) threat generation system","authors":"R. Smith, R. Taylor","doi":"10.1109/AERO.1994.291198","DOIUrl":"https://doi.org/10.1109/AERO.1994.291198","url":null,"abstract":"The Benefield Anechoic Facility (BAF) is part of the Avionics Test and Integration Complex located at the Air Force Flight Test Center, Edwards AFB, California. The mission of the BAF is to support installed systems testing for avionics test programs requiring a large, shielded chamber with radio frequency (RF) absorption capability that simulates free space. The BAF houses a unique threat generation system that is used to provide RF stimuli for avionics and electronic warfare systems.<<ETX>>","PeriodicalId":223269,"journal":{"name":"Proceedings of 1994 IEEE Aerospace Applications Conference Proceedings","volume":"15 3","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1994-02-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114036012","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
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