Title :
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
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;
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
DOI :
10.1109/MSNMC.2014.6979729
