نتایج جستجو برای: inertial navigation

تعداد نتایج: 68629  

2008
Pavel Davidson Jani Hautamäki Jussi Collin

This paper presents the development of GPS based navigation system for portable devices at Tampere University of Technology. The objective was to develop a fully integrated system using MEMS inertial sensors with price range of US$ 10-15 for the set of inertial sensors combined with low-update rate GPS measurements. This system doesn’t require vehicle installation and can be easily transferred ...

Journal: :ISPRS Int. J. Geo-Information 2015
Raymond Hung Bruce A. King Wu Chen

Mobile Laser Scanning (MLS) systems are widely applied for spatial data collection and support applications in many aspects. In recent years, MLS technology had been introduced to railway applications and greatly enhanced the spatial detail and efficiency when compared to traditional approaches. However, the advance of MLS technology is not completely applied to railway environment. Typical MLS...

2010
George T. Schmidt Richard E. Phillips Charles Stark

An inertial navigation system (INS) exhibits relatively low noise from second to second, but tends to drift over time. Typical aircraft inertial navigation errors grow at rates between 1 and 10 nmi/h (1.8 to 18 km/h) of operation. In contrast, Global Positioning System (GPS) errors are relatively noisy from second to second, but exhibit no long-term drift. Using both of these systems is superio...

Journal: :DEStech Transactions on Engineering and Technology Research 2019

2012
Aboelmagd Noureldin Justin Armstrong Ahmed El-Shafie Tashfeen B. Karamat Donald McGaughey Michael J. Korenberg Aini Hussain

In both military and civilian applications, the inertial navigation system (INS) and the global positioning system (GPS) are two complementary technologies that can be integrated to provide reliable positioning and navigation information for land vehicles. The accuracy enhancement of INS sensors and the integration of INS with GPS are the subjects of widespread research. Wavelet de-noising of I...

Journal: :J. Aerospace Inf. Sys. 2013
Allen Wu Eric N. Johnson Michael Kaess Frank Dellaert Girish Chowdhary

A vision-aided inertial navigation system that enables autonomous flight of an aerial vehicle in GPS-denied environments is presented. Particularly, feature point information from a monocular vision sensor are used to bound the drift resulting from integrating accelerations and angular rate measurements from an Inertial Measurement Unit (IMU) forward in time. An Extended Kalman filter framework...

Journal: :JACIC 2005
Allen Wu Eric N. Johnson Alison A. Proctor

Many onboard navigation systems use the Global Positioning System to bound the errors that result from integrating inertial sensors over time. Global Positioning System information, however, is not always accessible since it relies on external satellite signals. To this end, a vision sensor is explored as an alternative for inertial navigation in the context of an Extended Kalman Filter used in...

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