کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
412153 679616 2010 13 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
The integration of strap-down INS and GPS based on adaptive error damping
موضوعات مرتبط
مهندسی و علوم پایه مهندسی کامپیوتر هوش مصنوعی
پیش نمایش صفحه اول مقاله
The integration of strap-down INS and GPS based on adaptive error damping
چکیده انگلیسی

The concept and results of integration of a strap-down inertial navigation system (INS) based on low-accuracy inertial sensors and the global positioning system (GPS) have been presented in this paper. This system is aimed for the purposes of navigation, automatic control, and remote tracking of land vehicles. The integration is made by the implementation of an extended Kalman filter (EKF) scheme for both the initial alignment and navigation phases. Traditional integration schemes (centralized and cascaded) are dominantly based on the usage of high-accuracy inertial sensors. The idea behind the suggested algorithm is to use low-accuracy inertial sensors and the GPS as the main source of navigation information, while the acceptable accuracy of INS is achieved by the proper damping of INS errors. The main advantage of integration consists in the availability of reliable navigation parameters during the intervals of absence of GPS data. The influence of INS error damping coefficients is different depending on the fact whether the moving object is maneuvering or is moving with a constant velocity at that time. It is proposed that INS error damping gain coefficients generally should take higher values always when GPS data are absent, while at the same time their values in the error model (EKF prediction phase) can be additionally adapted according to the actual values of vehicle acceleration. The analysis of integrated navigation system performances is made experimentally. The data are acquired along the real land vehicle’s trajectory while the intervals of absence of GPS data are introduced artificially on the parts characterized both by maneuver and by constant velocity.

Research highlights
► The intervals of absence of GPS signal should be covered by correct INS outputs;
► The 15-th order optimal estimator of INS errors is used in the case of low-accuracy inertial sensors;
► INS error damping is introduced with the adaptation of damping factors;
► This adaptation is regarding to the presence/absence of GPS signal and the vehicle’s maneuver.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Robotics and Autonomous Systems - Volume 58, Issue 10, 31 October 2010, Pages 1117–1129
نویسندگان
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