Results 21 to 30 of about 1,081 (178)
Research on Algorithms for Multi‐Vector Attitude Determination
Various attitude estimation methods are based on an optimization problem posed in 1965 by Grace Wahba, which is called Wahba’s problem in the field of attitude estimation. As a key for attitude determination, many different algorithms for minimizing Wahba’s loss function have been proposed in the past 60 years.
Yilin Liu +4 more
wiley +1 more source
As an emerging means of transportation for the intelligent transportation system (ITS) in aviation and aerospace, hypersonic cruise vehicles (HCVs) have received numerous research interests during the past several decades. However, the navigation and positioning strictly limit the progress and application of HCVs due to their special characteristics on
Fei Xu +3 more
wiley +1 more source
As a common integrated navigation system, the strapdown inertial navigation system (SINS)/global positioning system (GPS) can estimate velocity and position errors well.
Songyin Cao, Honglian Gao, Jie You
doaj +1 more source
Novel Special Orthogonal Group Optimization for Coarse Alignment Method of SINS on a Rocking Base
In order to solve the coarse alignment problem of the strapdown inertial navigation system on a rocking base, a fast coarse alignment method using the Special Orthogonal Group optimization has been proposed in this paper. In this method, based on the alignment idea of tracing gravitational apparent motion in inertial frame, the model of coarse ...
Fujun Pei +4 more
wiley +1 more source
In recent years, along with microelectromechanical (MEMS) technique and wireless body area network (WBAN), wearable health monitoring systems have emerged. With sustainability posture detection technique, people pay more and more attention to mankind posture detection.
Wei Jin, Xin Ning
wiley +1 more source
Алгоритм управления беспилотными летательными аппаратами в процессе визуального сопровождения объектов с изменяемой траекторией движения [PDF]
The purpose of the research was to create an algorithm for determining and correcting the output parameters of the navigation module and the flight-navigation complex of unmanned aerial vehicles which provides control of an aviation gyro-stabilized ...
A. A. Adnastarontsau +15 more
core +2 more sources
Robust adaptive Kalman filter for strapdown inertial navigation system dynamic alignment
Abstract The measurement noise covariance R plays a vital role in the Kalman filter (KF) algorithm. Traditionally, a constant R is obtained by experience or experiments. However, the KF cannot achieve optimal estimation using constant R under non‐Gaussian conditions.
Bing Zhu +4 more
wiley +1 more source
Singular value decomposition-based robust cubature Kalman filtering for an integrated GPS/SINS navigation system [PDF]
A new nonlinear robust filter is proposed in this paper to deal with the outliers of an integrated Global Positioning System/Strapdown Inertial Navigation System (GPS/SINS) navigation system.
Chen +10 more
core +3 more sources
Analysis of the Strapdown Inertial Navigation System (SINS) Error Genesis
Abstract Analysis and simulation of the Strapdown Inertial Navigation System (SINS) error genesis revealed that the East Feedback Contour has the greatest influence on the development of an error in this model, and angular velocity sensor Δω𝒚 is the critical element.
Trifonovs-Bogdanovs, Pjotrs +1 more
openaire +2 more sources
Abstract The issue of non‐linear robust state estimation in the integration of a strapdown inertial navigation system and global positioning system is addressed in this study. Based on the cubature Kalman filtering frame, a non‐linear robust filter called a robust cubature Kalman filter (RCKF) was introduced to address the outliers and the inaccurate ...
Zhangjun Yu +4 more
wiley +1 more source

