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

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PAALS: precision accelerometer alignment and leveling system PAALS:精密加速度计对准和调平系统
R. Leonardson
{"title":"PAALS: precision accelerometer alignment and leveling system","authors":"R. Leonardson","doi":"10.1109/PLANS.1990.66229","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66229","url":null,"abstract":"A description is given of the precision accelerometer alignment and leveling system (PAALS), a high-performance microcontroller-corrected accelerometer triad that outputs acceleration (ft/s/sup 2/) via MIL-STD-1553BN communications. Combined tight-packaging, high-reliability, and high-performance requirements were the main design drivers. The key system elements are QA-700 Accelerometers, an Intel 80C 196 microcontroller, custom digital ASIC (application-specific integrated circuit), custom hybrid, and dual redundant MIL-STD-1533B communication components. For high performance, the QA-700 accelerometers are thermally modeled (third-order) for bias, scale factor, and alignment. The hybrid (three digitizers) is thermally modeled (third-order) for scale factor and offset, as well as input linearity. Extensive FDIRR (fault detection, indication, reporting, and recording) has been incorporated for supportability and maintainability.<<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":"128901301","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
Testing a decentralized filter for GPS/INS integration 测试GPS/INS集成的分散式滤波器
M. Wei, K. Schwarz
{"title":"Testing a decentralized filter for GPS/INS integration","authors":"M. Wei, K. Schwarz","doi":"10.1109/PLANS.1990.66210","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66210","url":null,"abstract":"A decentralized Kalman filter strategy is presented and applied to GPS/INS (Global Positioning System/inertial navigation system) integration. Two Kalman filters are used. One is a local filter, processing GPS data and providing locally best estimates of position and velocity. The second is an INS filter which uses the results from the GPS filter as updates to the estimates obtained from the inertial data. Because of the high short-term accuracy of the inertial system, the position results from INS can be used for cycle slip detection and correction. The major advantages of this method are the flexible combination of GPS and INS and the simplicity of the implementation. Compared to centralized filtering, the decentralized filter gives globally the same optimal estimation accuracy as the centralized Kalman filter. The accuracy does not deteriorate when a suboptimal cascaded filter is used, which has some advantages in terms of computational efficiency. Extension of this method to more sensors is straightforward. Numerical results are used to illustrate the salient features of the method.<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"44 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":"117339524","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: 77
VLS: a DTOA system for position location VLS:用于定位位置的DTOA系统
W.E. Sagey, W. R. Fried
{"title":"VLS: a DTOA system for position location","authors":"W.E. Sagey, W. R. Fried","doi":"10.1109/PLANS.1990.66240","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66240","url":null,"abstract":"A vehicle location system (VLS) is described. It is a derivative of the military position location and reporting system and offers higher accuracies and a lower vehicle electronics cost than any comparable system. The original design concept envisioned a satellite-based implementation in the radio determination satellite service band at 1.6 GHz for the location of surface vehicles on a nationwide basis. A second version of the system has evolved which is suitable for the tracking of aircraft to accuracies of 30 m in areas of interest and achieves those accuracies through the use of auxiliary ground enhancement stations. Terrestrial adaptations utilizing the cellular telephone infrastructure are in the exploratory phase. Experimental systems suitable for local area coverage have reached the field evaluation engineering model state. Some preliminary field test results are presented. Geostationary satellites are often optimal, though very good results are obtained for local systems without them.<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"1245 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":"131689614","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
Development of a new data link for the GPS range system GPS测距系统新型数据链的研制
R. F. Quick, K. Gilhousen, M. Birnbaum, J. Blanda
{"title":"Development of a new data link for the GPS range system","authors":"R. F. Quick, K. Gilhousen, M. Birnbaum, J. Blanda","doi":"10.1109/PLANS.1990.66192","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66192","url":null,"abstract":"The GPS (Global Positioning System) range data link is being developed for the primary purpose of supporting GPS position data collection and processing. The authors discuss the data-link message capacity required to support the generation and downlinking of GPS navigation solutions, using several range differential methods. They also discuss data link networking, with emphasis on the features required to provide high-reliability message transmission while downlinking data from highly dynamic aircraft. Support of GPS navigation in the test and training range environment requires the uplinking of receiver control messages and (for some solution methods) differential correction data. Downlink data include unprocessed receiver data and/or navigation solutions, plus receiver status data. The data link provides a nominal throughput of 200000 b/s, the greatest part being used for downlink data. To accommodate the largest GPS message blocks planned, data are transmitted in 736-b packets. Packet transmission is governed by a time-division multiple-access protocol, using 330 packet slots per second, of which approximately 280 are available for GPS data uplink and downlink. Integration of the data link into range data processing and control facilities is discussed, along with data link features allowing cooperative interoperation among adjacent ranges.<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"46 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":"133963630","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
Precision gravity measurement utilizing Accelerex vibrating beam accelerometer technology 利用加速度振动梁加速度计技术进行精密重力测量
B. Norling
{"title":"Precision gravity measurement utilizing Accelerex vibrating beam accelerometer technology","authors":"B. Norling","doi":"10.1109/PLANS.1990.66221","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66221","url":null,"abstract":"Tests run using Sundstrand vibrating beam accelerometers to sense microgravity are described. Lunar-solar tidal effects were used as a highly predictable signal which varies by approximately 200 billionths of the full-scale gravitation level. Test runs of 48-h duration were used to evaluate stability, resolution, and noise. Test results on the Accelerex accelerometer show accuracies suitable for precision applications such as gravity mapping and gravity density logging. The test results indicate that Accelerex technology, even with an instrument design and signal processing approach not optimized for microgravity measurement, can achieve 48-ngg (1 sigma ) or better accuracy over a 48-h period. This value includes contributions from instrument noise and random walk, combined bias and scale factor drift, and thermal modeling errors as well as external contributions from sampling noise, test equipment inaccuracies, electrical noise, and cultural noise induced acceleration.<<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":"134074614","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: 5
Evaluation of controller tools for conducting MLS curved approaches to New York's JFK Airport 对管制员工具进行MLS曲线进近到纽约肯尼迪机场的评估
A. Smith, C. Shively, R. Tarakan, G. Dorfman, K. Markin
{"title":"Evaluation of controller tools for conducting MLS curved approaches to New York's JFK Airport","authors":"A. Smith, C. Shively, R. Tarakan, G. Dorfman, K. Markin","doi":"10.1109/PLANS.1990.66184","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66184","url":null,"abstract":"The authors describe the simulation and evaluation of an automation aid for helping air traffic controllers deal with aircraft that might fly MLS (microwave landing system) curved approaches to John F. Kennedy International Airport (JFK) in New York. In the scenario studied, aircraft with appropriate MLS equipment would fly a curved approach to JFK's runway 13R, while other aircraft would fly the currently used straight-in ILS (instrument landing system) approach to parallel runway 13L. To deal with the possible case of an MLS aircraft that blunders toward the ILS path, this scenario requires controllers to maintain an appropriate stagger between aircraft on the two approaches. The automation aid investigated is a projected image of the controller's display. Controllers from the New York Terminal Radar Approach Control Facility have participated in simulated traffic scenarios to evaluate this aid. Initial observations are given.<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"24 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":"125952427","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
Integrated inertial navigation system/Global Positioning System (INS/GPS) for manned return vehicle autoland application 用于载人返回飞行器自动着陆的综合惯性导航系统/全球定位系统(INS/GPS)
K. Braden, C. Browning, H. Gelderloos, F. Smith, C. Marttila, L. Vallot
{"title":"Integrated inertial navigation system/Global Positioning System (INS/GPS) for manned return vehicle autoland application","authors":"K. Braden, C. Browning, H. Gelderloos, F. Smith, C. Marttila, L. Vallot","doi":"10.1109/PLANS.1990.66160","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66160","url":null,"abstract":"It is noted that with the development of the International Space Station Freedom, people will permanently live in space and require routine access and an assured crew return capability in case of emergencies in space. The extended duration in space requires a manned return vehicle that is less demanding on the crew and provides an autonomous deorbit, entry, and autoland capability. The authors discuss an autoland capability with an integrated differential GPS/INS that provides the required position and velocity accuracies without the need for tactical aircraft navigation (TACAN) and microwave landing system (MLS) navigation aides. Simulation results are used to demonstrate the feasibility of autoland using differential GPS aided with a high-precision altimeter. This concept applies to several manned space applications, such as Assured Crew Return Vehicle (ACRV), Assured Shuttle Availability (ASA), Advanced Manned Launch System (AMLS), and National Aerospace Plane (NASP), and to unmanned return vehicles such as the Propulsion Avionics Module (P/AM).<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"60 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":"122250569","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: 10
A low-cost GPS inertial guidance (GPSIG) for space boosters 用于太空助推器的低成本GPS惯性制导(GPSIG)
S. C. Maki
{"title":"A low-cost GPS inertial guidance (GPSIG) for space boosters","authors":"S. C. Maki","doi":"10.1109/PLANS.1990.66174","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66174","url":null,"abstract":"The GPS (Global Positioning System) application requirements for a variety of space vehicles, including the Space Transport Vehicle (STV), the Orbital Maneuvering Vehicle (OMV), the heavy lift launch vehicles of the Advanced Launch Systems (ALS) family and the Shuttle C (cargo), space platforms, and future manned vehicles, are summarized. GPS usage on unmanned space boosters is examined in greater depth. The requirements in the areas of performance, operational constraints, redundancy/reliability, implementation, and life cycle cost are detailed. Variations from the typical GPS/INS (inertial navigation system) integration approach are presented, including deletion of some inertial sensors, various types of inertial sensors, and multiplexed and separate channel receivers.<<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":"117153932","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
Demonstration of a ring laser gyro system for pointing and stabilization applications 用于指向和稳定应用的环形激光陀螺系统的演示
R.G. Majure
{"title":"Demonstration of a ring laser gyro system for pointing and stabilization applications","authors":"R.G. Majure","doi":"10.1109/PLANS.1990.66180","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66180","url":null,"abstract":"A system specifically designed to meet the requirements of the pointing and stabilization community is presented. Such applications include synthetic aperture radar (SAR) motion compensation and infrared sensor stabilization. Requirements peculiar to this application are discussed and contrasted with traditional inertial navigation requirements. Pointing and stabilization demand consideration of requirements such as high bandwidth, low noise, minimal data latency, dither effects, reference alignment, minimization of size, near-instantaneous turn-on, and analysis of structural resonances. The GG1320 RLG (ring laser gyro) was chosen for this application since it provided the necessary accuracy and could be contained in a small volume. Test results are presented indicating the performance of the IMU (inertial measurement unit). Testing techniques are also discussed and contrasted with traditional inertial navigation system testing. Results indicate that the GG1320 RLG IAU (inertial attitude unit) is capable of meeting the requirements of the pointing and stabilization community. Current and future development activities are discussed relative to performance enhancement, and further applications and requirements are identified.<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"66 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":"130633334","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
Geostationary repeaters: a low cost way to enhance civil user performance of GPS and GLONASS 静止中继器:提高GPS和GLONASS民用用户性能的低成本方法
J. Nagle, G.V. Kinal
{"title":"Geostationary repeaters: a low cost way to enhance civil user performance of GPS and GLONASS","authors":"J. Nagle, G.V. Kinal","doi":"10.1109/PLANS.1990.66149","DOIUrl":"https://doi.org/10.1109/PLANS.1990.66149","url":null,"abstract":"Inmarsat proposes to implement a set of geostationary repeaters operating in the navigation L-band (approximately 1575 MHz) to serve as an overlay to the GPS (Global Positioning System) and GLONASS (the Soviet global navigation satellite system). One major motivation for the overlay is the need expressed by the aeronautical community for an independent, quick response (10 s) external integrity channel. An additional advantage of a navigation band solution is that it would be received by (virtually) unmodified GPS and/or (slightly) modified GLONASS receivers. The integrity, coverage, availability, and timing enhancements that are possible from geostationary augmentation to GPS are discussed. A description of the Inmarsat pseudonoise (PN) test program where GPS-compatible PN-signal formats are transmitted through current Inmarsat satellites is presented to demonstrate the simplicity and practicality of the geostationary repeater augmentation technique.<<ETX>>","PeriodicalId":156436,"journal":{"name":"IEEE Symposium on Position Location and Navigation. A Decade of Excellence in the Navigation Sciences","volume":"30 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":"132711431","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
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