IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences最新文献

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Motion compensation for ASTOR long range SAR ASTOR远程SAR的运动补偿
John S. A. Hepburn, C. Doyle
{"title":"Motion compensation for ASTOR long range SAR","authors":"John S. A. Hepburn, C. Doyle","doi":"10.1109/PLANS.1990.66178","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66178","url":null,"abstract":"The United Kingdom Ministry of Defence is conducting a long range synthetic aperture radar (SAR) technology demonstrator programme (TDP) in support of their airborne stand-off radar programme. A major goal is to develop a high-resolution airborne SAR with both strip map and spotlight modes. To attain the image quality objectives of the project, it is essential that very accurate motion compensation be applied to the radar returns to reduce image degradation, caused by spurious antenna phase center motion, to acceptable levels. The SAR motion compensation system (SARMC) includes a master inertial navigation system located near the center of mass of the host aircraft and a slaved strapdown inertial measurement unit mounted on the back of the radar antenna, as well as Doppler velocity and barometric and radar altimeters. The performance of the SARMC has been evaluated both by analysis and computer simulation. These evaluations accounted for all major system error sources, including errors associated with sensors, transfer alignment, and computation, with the system operating in an environment of moderate atmospheric turbulence. Results from these evaluations are presented.<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1990-03-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122202311","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
Ashtech XII GPS technology Ashtech十二GPS技术
J. Ashjaee
{"title":"Ashtech XII GPS technology","authors":"J. Ashjaee","doi":"10.1109/PLANS.1990.66175","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66175","url":null,"abstract":"Several enhancements of GPS (Global Positioning System) technology are presented, including new data processing algorithms, enhanced application techniques, more hardware capabilities, and reduction in size and power consumption. The use of Doppler measurements for instantaneous (every one second) stationary position fixes is introduced. This technique has the potential of reducing the effect of selective availability in static point positioning. It is shown that the combination of Doppler and code phase measurements can provide two-dimensional deterministic static position fixes (and time) with only two satellites. It can also provide three-dimensional position fixes (and time) with three satellites. The proposed techniques expand the usage of GPS in areas with low satellite visibility and in the interim period while the GPS satellite constellation is not complete. The notion of multiple ramp smoothing of code phase with integrated Doppler is introduced. The results of implementation of this technique in Ashtech XII receivers for real-time differential GPS is given. Minimizing the errors in the use of GPS for aerial photogrammetry applications is discussed. A new technique implemented in Ashtech XII GPS is presented. A new generation of GPS receiver (Ashtech M-XII) is introduced. It is capable of performing precision survey, navigation, and time transfer. The 12-channel receiver uses a higher level of hardware integration. The results of Ashtech XII dual frequency receivers on the FGCC (Federal Geodetic Control Committee) test network are presented.<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"50 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1990-03-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122897238","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
Global Positioning System (GPS) autonomous navigation 全球定位系统(GPS)自主导航
M. Ananda, H. Bernstein, K. Cunningham, W. Feess, E.G. Stroud
{"title":"Global Positioning System (GPS) autonomous navigation","authors":"M. Ananda, H. Bernstein, K. Cunningham, W. Feess, E.G. Stroud","doi":"10.1109/PLANS.1990.66220","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66220","url":null,"abstract":"A system description, a discussion of design issues, and performance results obtained from the Aerospace Corporation simulation of the GPS autonomous navigation system (ANS) concept are given. Analysis methods, physical models, and pertinent equations are presented. Measurement data are realistically simulated and include the effects of all known environmental and hardware phenomena affecting performance. Performance under nominal and anomalous conditions (satellite failures) and in nuclear environments is described. Unobservable errors which degrade performance are discussed. Preliminary studies show that the full constellation system is measurement rich. A simple scheme such as rejecting low signal-to-noise ratio or high delay measurements will probably be a satisfactory design response to distortion due to scintillation in the enhanced environment.<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1990-03-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"124680311","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: 97
Impact of navigation accuracy on the intervention rate in a highly automated air traffic control system 高度自动化空中交通管制系统中导航精度对干预率的影响
M.J. Rockman, R. Braff
{"title":"Impact of navigation accuracy on the intervention rate in a highly automated air traffic control system","authors":"M.J. Rockman, R. Braff","doi":"10.1109/PLANS.1990.66213","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66213","url":null,"abstract":"Progress in navigation technology is expected to bring about a lower air traffic control (ATC) intervention rate than the rate that could be expected based upon today's navigation and flight control capabilities. The extent to which this may occur is quantified, and additional possible benefits, such as increasing air traffic throughput and intervening earlier in potential loss of separation between aircraft, are discussed. A prototypic aircraft-aircraft encounter is defined. It includes a simple intervention-decision rule which attempts to capture the prudence practiced by today's air traffic controllers, and which typifies one type of decision rule presently under consideration for use in a future automated ATC system such as AERA 3. This rule is applied to an operational environment where GPS (Global Positioning System) is employed to navigate user-preferred routes.<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"23 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1990-03-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"131799965","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
A near real-time gravity gradiometer data review system 近实时重力梯度数据审查系统
S.J. Brzezowski, J.A. Cochand, L. Murano, J. White, J. L. Wylie, W. Heller
{"title":"A near real-time gravity gradiometer data review system","authors":"S.J. Brzezowski, J.A. Cochand, L. Murano, J. White, J. L. Wylie, W. Heller","doi":"10.1109/PLANS.1990.66223","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66223","url":null,"abstract":"A graphics-based data analysis system was developed for the review, in near real time, of output from a prototype gravity gradiometer survey system (GGSS). Analysis of data from initial GGSS tests had identified the need for additional data monitoring to supplement the associated baseline procedures built into the GGSS. Shakedown exercises of the PC-based data review system (DRS) took place during GGSS Rail Garrison Peacekeeper testing in the winter of 1988. Based on the review of nearly 200 h of data stored on over 100 magnetic tapes, DRS findings indicate that sufficient subsets of data were collected along the 560-mile route between Albuquerque, New Mexico and Dodge City, Kansas to support the subsequent estimation of gravity disturbances.<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"25 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1990-03-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133306902","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
A fast and low-cost validation technique for ILS and MLS 一种快速、低成本的ILS和MLS验证技术
P. Mahapatra, M. Poulose
{"title":"A fast and low-cost validation technique for ILS and MLS","authors":"P. Mahapatra, M. Poulose","doi":"10.1109/PLANS.1990.66183","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66183","url":null,"abstract":"A feasibility study of evaluating site effects on ILS (instrument landing system) and MLS (microwave landing system) using analytical and computational techniques is presented. The problem of site effect evaluation is divided into three stages: terrain modeling, ray tracing, and field evaluation. Innovative techniques are introduced at each stage to make the model versatile enough to handle most general terrain contours and surface conditions and also reduce computational requirements to a minimum. The result is a scheme that can be used to evaluate most terrain types on a mini/microcomputer. Specifically, it is shown that, using a simple two-dimensional multiwedge model of the terrain (i.e. no variation of terrain height in the third dimension), it is possible to obtain accurate estimates of the glideslope parameters by simulating procedures similar to those specified by ICAO (the International Civil Aviation Organization). The computational results have been visualized by comparison with actual data from flight tests. A summary of results for actual sites is presented.<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"35 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1990-03-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133320635","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
Determination of precise position of a moving vehicle with GPS 用GPS确定移动车辆的精确位置
C. Goad
{"title":"Determination of precise position of a moving vehicle with GPS","authors":"C. Goad","doi":"10.1109/PLANS.1990.66187","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66187","url":null,"abstract":"Global Positioning System (GPS) phase data were collected from a receiver moving on a vehicle whose position and velocity were being monitored by another precise tracking system. Centimeter-level agreement was found between the two systems. Except for initial positioning or alignment biases of 2-3 cm, root-mean-square (RMS) values were often less than 1 cm. It is thus concluded that precise GPS measurements of carrier phase can be used to determine relative position even while in motion.<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"8 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1990-03-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"121727455","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
The next frontier for strapdown RLG inertial systems. Precision navigation 捷联式RLG惯性系统的下一个前沿领域。精确导航
R. Upton, W. Miller
{"title":"The next frontier for strapdown RLG inertial systems. Precision navigation","authors":"R. Upton, W. Miller","doi":"10.1109/PLANS.1990.66225","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66225","url":null,"abstract":"Honeywell research and development projects directed at improvements in the design, building, and testing of RLG (ring laser gyro) strapdown systems are reviewed. Some of the performance standards being set with current hardware are discussed, as are a number of the known error sources existing in these systems along with candidate solutions, the analysis and test results upon which precision navigation performance projections are based, and plans to demonstrate the feasibility of a precision pure strapdown RLG system. Based upon current performance, reasonable projections and analysis, and laboratory test data, it is anticipated that strapdown RLG systems can deliver performance consistent with the precision requirements of SNU 84-3 (0.2 nm/h after a precision-extended time-alignment) while retaining the major advantages that the pure strapdown mechanization offers.<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"39 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1990-03-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116326738","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
Ring laser gyro applications for tactical missiles: the Army TACMS solution 环形激光陀螺应用于战术导弹:陆军TACMS解决方案
G. Curran, D.J. Engelken
{"title":"Ring laser gyro applications for tactical missiles: the Army TACMS solution","authors":"G. Curran, D.J. Engelken","doi":"10.1109/PLANS.1990.66226","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66226","url":null,"abstract":"The Honeywell H700-3A ring laser gyro missile guidance set (AN/DJW-51) provides navigation, guidance, autopilot, weapons dispensing, and communications functions for the US Army TACMS missile in a low-initial-cost and low-life-cycle-cost package. It is primarily the use of low-cost inertial sensors which make the use of a ring laser gyro navigation system feasible in the tactical missile market. The H700-3A ring laser gyro missile guidance set has proven to be a low-cost, high-accuracy guidance and navigation system for the deep-strike Army missile weapons system. This has been borne out by a highly successful test program of 26 missile flights. The components of the missile guidance set are described in detail.<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"11 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1990-03-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114986786","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: 12
Application of electronic chart systems in the prevention of ship's groundings 电子海图系统在防止船舶搁浅中的应用
H. Lanziner, D. Michelson
{"title":"Application of electronic chart systems in the prevention of ship's groundings","authors":"H. Lanziner, D. Michelson","doi":"10.1109/PLANS.1990.66157","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66157","url":null,"abstract":"It is noted that despite glowing recommendations from users, the market for electronic charts has not grown at the rate that many had expected. Some of the possible reasons for this are considered, and recommendations for corrective action are presented. One reason may be that shipping is a conservative and very cost-conscious industry; because ships have sailed without electronic charts in the past, it is difficult to convince owners that it is necessary to rush out and have one installed. The situation is compounded by the lack of international standards for electronic chart display (ECDIS) systems and, indeed, by the lack of international regulations requiring the use of ECDIS systems on board ship. However, it is generally recognized that electronic charts provide the only reasonable method of presenting precise position information to masters or pilots during critical maneuvering in restricted waters such as harbors and harbor approaches. As hardware becomes more sophisticated and capable, as experience is accumulated, and as precise positioning systems (e.g. GPS and RANAV) become widely available during the 1990s, it is expected that the market for electronic charts will grow tremendously.<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"75 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1990-03-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"124280152","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
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