Integrated aircraft navigation system

Author

Malysheva, J.O.

Author_Institution

Fac. of Aviation & Space Syst., Nat. Tech. Univ. of Ukraine Kyiv Polytech. Univ., Kiev, Ukraine

fYear

2013

fDate

15-17 Oct. 2013

Firstpage

169

Lastpage

172

Abstract

The paper describes the integrated aircraft navigation system, which includes the strapdown inertial navigation system (SINS), GPS receiver, optical horizon sensor and magnetometer. The integration algorithm for such system based on the Kalman filtering is represented. Application of this algorithm allows to improve the accuracy of the aircraft motion parameter estimation. For an optical horizon sensor a self-contained horizon recognition algorithm that enables real-time aircraft attitude determination relative to the horizon line is developed. A scaled-down simulation and performance analysis of the operation of the integrated navigation system is carried out.

Keywords

Global Positioning System; Kalman filters; aircraft control; aircraft navigation; attitude control; inertial navigation; magnetometers; motion control; optical sensors; GPS receiver; Kalman filtering; SINS; aircraft motion parameter estimation; integrated aircraft navigation system; integration algorithm; magnetometer; optical horizon sensor; real-time aircraft attitude determination; self-contained horizon recognition algorithm; strapdown inertial navigation system; Aircraft navigation; Estimation; Global Positioning System; Magnetometers; Optical filters; Optical sensors; Silicon compounds; Kalman filtering; horizon detection; navigation system; optical sensor; strapdown inertial navigation syste;

fLanguage

English

Publisher

ieee

Conference_Titel

Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD), 2013 IEEE 2nd International Conference

Conference_Location

Kiev

Print_ISBN

978-1-4799-3305-1

Type

conf

DOI

10.1109/APUAVD.2013.6705316

Filename

6705316