Results 171 to 180 of about 1,636 (211)
Some of the next articles are maybe not open access.

Improvement of strapdown inertial navigation using PDAF

IEEE Transactions on Aerospace and Electronic Systems, 1999
A new application of PDAF (probabilistic data association filter) for improving the accuracy of autonomous strapdown inertial navigation systems (SINS) is presented. The proposed method is a terrain-aided navigation (TAN) algorithm based on landmark detection combined with a classical SINS.
openaire   +1 more source

A New Mathematical Formulation for Strapdown Inertial Navigation

IEEE Transactions on Aerospace and Electronic Systems, 1971
A differential equation is developed for the orientation vector relating the body frame to a chosen reference frame. The time derivative of this vector is the sum of the inertially measurable angular velocity vector and of the inertially nonmeasurable noncommutativity rate vector.
openaire   +1 more source

New techniques for initial alignment of strapdown inertial navigation system

Journal of the Franklin Institute, 2009
zbMATH Open Web Interface contents unavailable due to conflicting licenses.
Shaolin Lü, Ling Xie, Jiabin Chen
openaire   +2 more sources

Correction of a Strapdown Inertial Navigation System During Descent in the Atmosphere

Mechanics of Solids, 2023
The article deals with the problem on determining the angular position during descent on an apparatus with low lift-drag ratio. A solution is presented using the least squares method, which reduces to determining the orientation quaternion using a system of linear algebraic equations.
openaire   +1 more source

Initial Alignment by Attitude Estimation for Strapdown Inertial Navigation Systems

IEEE Transactions on Instrumentation and Measurement, 2015
This paper derives a novel initial alignment method for the strapdown inertial navigation system (SINS), which transforms the attitude alignment into an attitude estimation problem. The process model of the proposed initial alignment method by attitude estimation is established by decomposition of the attitude matrix.
Lubin Chang, Jingshu Li, Shengyong Chen
openaire   +1 more source

Strapdown Inertial Navigation System Algorithms Based on Geometric Algebra

Advances in Applied Clifford Algebras, 2012
zbMATH Open Web Interface contents unavailable due to conflicting licenses.
Wu, Dimin, Wang, Zhengzhi
openaire   +2 more sources

Strapdown inertial navigation system of pendulum type

Mechanics of Solids, 2014
We consider two implementations of an isotropic oscillator to be used in the construction of a strapdown inertial system of new type [1]. The first implementation is a contact-free suspension of an electrically conductive ball used in electrostatic gyros, and the second implementation is a 3D combination of elastic constraints holding a mass point.
openaire   +1 more source

In-Motion Filter-QUEST Alignment for Strapdown Inertial Navigation Systems

IEEE Transactions on Instrumentation and Measurement, 2018
By analyzing the error models of the measured vectors of the gravitational apparent motion, an in-motion filter-QUEST alignment method only with the inertial measurement unit is presented in this paper. The contribution of the proposed method lies in constructing the in-motion model of the measured vectors of the gravitational apparent motion and ...
Xiang Xu 0004   +3 more
openaire   +1 more source

Strapdown inertial navigation system of a rotating carrier

2017 24th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS), 2017
The paper deals with a strapdown inertial navigation system (SINS) of a rotating carrier (RC) characterized by a high roll speed and rather slow oscillations in the yaw and pitch angles. It is shown that it is expedient for an RC to develop four orientation parameters: traditional yaw angles, pitch and trigonometric functions of the sine, cosine of the
openaire   +1 more source

Basic principles of strapdown inertial navigation systems

2004
The previous chapter has provided some insight into the basic measurements that are necessary for inertial navigation. For the purposes of the ensuing discussion, it is assumed that measurements of specific force and angular rate are available along and about axes which are mutually perpendicular.
openaire   +1 more source

Home - About - Disclaimer - Privacy