IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences最新文献_第8页

Estimation of error correlation distance for differential GPS operation 差分GPS操作误差相关距离估计

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI: 10.1109/PLANS.1990.66203

G. Harkleroad, W. Tang, N. Johnson

引用次数: 9

Applying kinematic GPS techniques at our nation's airports 运动学GPS技术在我国机场的应用

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI: 10.1109/PLANS.1990.66186

B.W. Remondi

引用次数: 2

START: a broad application spectrum gyro for the 1990s 开始:为20世纪90年代广泛应用的陀螺仪

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI: 10.1109/PLANS.1990.66151

D. G. Harris

引用次数: 1

The use of INS/GPS in a highway survey system INS/GPS在公路测量系统中的应用

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI: 10.1109/PLANS.1990.66208

D. Lapucha, K. Schwarz, M. Cannon, H. Martell

引用次数: 18

Airborne gravimetry and the Global Positioning System 航空重力测量和全球定位系统

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI: 10.1109/PLANS.1990.66188

A. Kleusberg, D. Peyton, D. Wells

引用次数: 21

A robust approach to reliable real-time Kalman filtering 一种可靠的实时卡尔曼滤波鲁棒方法

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI: 10.1109/PLANS.1990.66227

P. McBurney

{"title":"A robust approach to reliable real-time Kalman filtering","authors":"P. McBurney","doi":"10.1109/PLANS.1990.66227","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66227","url":null,"abstract":"A complete approach to reliable, robust, and adaptive Kalman filtering is presented. It has applications in all types of navigation systems. The starting point is a measurement editing and filter divergence protection scheme based on measurement residuals and their expected statistics. Rather than simply increasing the white measurement noise variance, certain error sources which are known to be present can be included in the filter model via a Schmidt-Kalman filter, which allows certain states to be considered without being estimated. This type of filter configuration has many advantages over the usual Kalman filter such as larger region of convergence, smoother transitions between over-determined solutions, and more conservative modeling when certain states are frozen, such as during clock or altitude hold. Details are given on how this type of filter can be used with a factorized covariance. The same statistics used for filter integrity are also used to assess how well the filter is tuned to a particular dynamic environment. A reasonable adaptive process noise matrix scheme based on these statistics is presented. Specific examples of the application of these techniques in Global Positioning System receiver are given.<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"51 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":"121100996","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: 15

GG1308 ring laser gyro inertial measurement systems: Honeywell's low-cost solution for tactical applications GG1308环形激光陀螺惯性测量系统:霍尼韦尔战术应用的低成本解决方案

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI: 10.1109/PLANS.1990.66224

J.M. Oelschlaeger, L.O. Thielman

{"title":"GG1308 ring laser gyro inertial measurement systems: Honeywell's low-cost solution for tactical applications","authors":"J.M. Oelschlaeger, L.O. Thielman","doi":"10.1109/PLANS.1990.66224","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66224","url":null,"abstract":"The GG1308 ring laser gyro (RLG) inertial measurement systems represent the smallest-volume, lightest-weight, and lowest-cost RLG systems. These systems are designed to provide the functions required for inertial guidance, aided or midcourse navigation, and vehicle stabilization and control to a wide variety of tactical missiles, standoff weapons, unmanned aerial vehicles, torpedoes, and manned rotorcraft. GG1308 inertial systems achieve their low cost as a result of several significant development thrusts. Low-cost inertial sensors must be utilized. The GG1308 RLG is a true design-to-cost device with producibility and the cost of parts, materials, assembly labor, and manufacturing automation being the dominant design drivers. Additionally, these GG1308 inertial systems use a commonality design approach. This philosophy has made it possible to develop several generic hardware elements which need only be repackaged to provide an inertial system in the form factor required for specific programs. It also provides the system with an adaptability and intelligence to improve its performance throughout its useful life by making software improvements which do not affect the hardware design or production process.<<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":"124359643","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

Pipeline geometry pigging: application of strapdown INS 管线几何清管:捷联式INS的应用

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI: 10.1109/PLANS.1990.66199

T. Porter, E.H. Knickmeyer, R. Wade

引用次数: 6

HRG strapdown navigator HRG捷联导航仪

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI: 10.1109/PLANS.1990.66164

J. Dickinson, C. R. Strandt

{"title":"HRG strapdown navigator","authors":"J. Dickinson, C. R. Strandt","doi":"10.1109/PLANS.1990.66164","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66164","url":null,"abstract":"A new technology gyro, the hemispherical resonator gyro (HRG), has been developed which is ideally suited to strapdown navigation systems. The instrument offers greater reliability than current sensors due to its inherent simplicity. A fault-tolerant navigation system has been developed as a technology testbed to exhibit the instrument's capabilities. A successful flight test program of the system was completed in late 1989. This fault tolerant navigation system is configured with six independent sensor channels consisting of paired gyros and accelerometers. Each sensor channel utilizes a microprocessor, programmed in C, to control sensor readout and compensate for thermal errors. A central navigation processor, programmed in Ada, combines data from the independent sensor channels to provide redundancy management and an optimized navigation solution. A dodecahedron mounting structure for the instrument cluster provides an optimum alignment of the redundant inertial axes. Redundancy management of the sensors is accomplished by an enhanced generalized likelihood test. Key features demonstrated for the HRG navigator are rapid reaction, operation over a wide temperature range, and navigation accuracy.<<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":"126789846","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

The advantages of velocity vector referencing in proportional navigation 速度矢量参考在比例导航中的优势

IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences Pub Date : 1990-03-20 DOI: 10.1109/PLANS.1990.66163

P. Mahapatra, U. S. Shukla

{"title":"The advantages of velocity vector referencing in proportional navigation","authors":"P. Mahapatra, U. S. Shukla","doi":"10.1109/PLANS.1990.66163","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66163","url":null,"abstract":"Two broad classes of proportional navigation laws are compared with regard to their implementation, analysis, and behavior. The first consists of laws such as the PPN (pure proportional navigation) laws, which are referenced relative to the pursuer velocity vector, and the second consists of line-of-sight (LOS) referenced laws such as TPN (true PN), GTPN (generalized TPN), and GGL (generalized guidance law). It is shown that the latter class has serious drawbacks in terms of implementation and trajectory behavior, which more than offset the limited advantage in analytical treatment exploited hitherto in the literature. Among the major drawbacks are forward acceleration and braking requirements which are difficult to achieve, relative inefficiency in the utilization of control effects, restrictions on initial conditions, for intercept, lack of robustness, and the possibility of unbounded acceleration. From a practical point of view, PPN is a superior guidance law to TPN and its generalizations. The only utility of the LOS-reference laws appears to be to serve as approximations to analyze the more practical and efficient PPN law and its variants.<<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":"129264204","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