MATHEMATICAL MODEL OF ACCELEROMETER ERRORS STRAPDOWN INERTIAL NAVIGATION SYSTEM

Authors

  • A. V. Rudyk National Aviation University

Keywords:

strapdown inertial navigation system, accelerometer, model errors, acceleration, speed, coordinate system

Abstract

The article shows that the model errors of strapdown inertial navigation system (SINS) allows us to estimate the overall accuracy of SINS errors specified accelerometers and gyroscopes or solve the inverse problem — to formulate the requirements for inertial sensors, provided the specified accuracy SINS. There has been received SINS error model, which consists of equations of errors in determining the speed and coordinates of the object location. SINS error model is needed in the development of the Kalman filter to solve the problems of multi-SINS with other navigation devices. There has been shown the generalized block diagram form SINS errors in the determination of the object parameters, according to which the accuracy of determining the linear speed and coordinates of the location where the error affects the orientation and SINS error value depends on the dynamics of motion of the object.

Author Biography

A. V. Rudyk, National Aviation University

Cand. Sc. (Eng.), Assistant Professor, Doctoral Candidate of the Chair of Computer-Assisted Electrical Engineering Systems and Technologies

References

1. Матвеев В. В. Инерциальные навигационные системы : учеб. пос. / В. В. Матвеев. — Тула : изд-во ТулГУ, 2012. — 199 с.
2. Барабанов О. О. Математические задачи дальномерной навигации / О. О. Барабанов, Л. П. Барабанова. — М. : Физматлит, 2007. — 272 с. — ISBN 978-5-9221-0874-4.
3. Анучин О. Н. Интегрированные системы ориентации и навигации для морских подвижных объектов / О. Н. Анучин, Г. И. Емельянцев. — СПб. : изд-во «Государственный Научный Центр Российской Федерации», 1999. — 357 с. — ISBN 5-90780-22-8.
4. Тяпкин В. Н. Методы определения навигационных параметров подвижных средств с использованием спутниковой радионавигационной системы ГЛОНАСС : монография / В. Н. Тяпкин, Е. Н. Гарин. — Красноярск : Сибирский феде-ральный университет, 2012. — 260 с. — ISBN 978-5-7638-2639-5.
5. Перов А. И. ГЛОНАСС. Принципы построения и функционирования / А. И. Перов, В. Н. Харисов. — М. : Радио-техника, 2010. — 800 с. — ISBN 978-5-88070-251-0.
6. Groves P. D. Principles of GNSS, Inertial and Multisensor Integrated Navigation Systems / P. D. Groves. — Artech House, 2008. — 505 p. — ISBN-13: 978-1-58053-255-6.
7. Woodman O. J. An introduction to inertial navigation / O. J. Woodman // Technical reports published by the University of Cambridge. — 2007. — № 696. — 37 р.

Downloads

Abstract views: 126

Published

2017-05-31

How to Cite

[1]
A. V. Rudyk, “MATHEMATICAL MODEL OF ACCELEROMETER ERRORS STRAPDOWN INERTIAL NAVIGATION SYSTEM”, Вісник ВПІ, no. 2, pp. 7–13, May 2017.

Issue

No. 2 (2017)

Section

Automation and information-measuring equipment

Metrics

Downloads

Download data is not yet available.

License

Authors who publish with this journal agree to the following terms:

  • Authors retain copyright and grant the journal right of first publication.
  • Authors are able to enter into separate, additional contractual arrangements for the non-exclusive distribution of the journal's published version of the work (e.g., post it to an institutional repository or publish it in a book), with an acknowledgment of its initial publication in this journal.
  • Authors are permitted and encouraged to post their work online (e.g., in institutional repositories or on their website) prior to and during the submission process, as it can lead to productive exchanges, as well as earlier and greater citation of published work (See The Effect of Open Access).