Combined sensor of angular parameters for small unmanned aerial vehicles

Author

Filyashkin, M.K.

Author_Institution

Aviation Comput.-Integrated Complexes Dept., Nat. Aviation Univ., Kiev, Ukraine

fYear

2014

fDate

14-17 Oct. 2014

Firstpage

53

Lastpage

58

Abstract

Are given principles of the combined sensor which measures the angular parameters and is used in inertial-satellite systems constructed by the method of compensation or based on the reduced Kalman filter. Measurement errors of angular orientation parameters are investigated by the proposed method with aircraft performing various maneuvers and with changing the acceleration and attitude.

Keywords

Kalman filters; acceleration; aircraft control; angular velocity measurement; artificial satellites; autonomous aerial vehicles; compensation; measurement errors; sensors; acceleration; aircraft; angular orientation parameters; angular parameter measurement; combined sensor; inertial-satellite systems; maneuvers; measurement error; reduced Kalman filter; small unmanned aerial vehicles; Acceleration; Accelerometers; Angular velocity; Earth; Gravity; Navigation; Silicon compounds; acceleration; accelerometer; angular orientation; angular velocity sensor; compensation scheme;

fLanguage

English

Publisher

ieee

Conference_Titel

Methods and Systems of Navigation and Motion Control (MSNMC), 2014 IEEE 3rd International Conference on

Conference_Location

Kiev

Print_ISBN

978-1-4799-6578-6

Type

conf

DOI

10.1109/MSNMC.2014.6979729

Filename

6979729