Journal of Projectiles, Rockets, Missiles and Guidance >
Attitude Estimation of Octorotor Aircraft Based on Information Fusion
Received date: 2015-04-15
Online published: 2025-05-30
In view of redundancy and load limitation of four rotor aircraft, the design of rotor aircraft was put forward A dynamic model of eight rotor aircraft was analyzed, its movement equation of state was established; UKF was designed to implement the aircraft attitude algorithm:Design of Kalman filter realized calculating speed and height of the aircraft. Theoretical analysis and simulation experiments show that the Kalman filtering algorithm can satisfy data calculation accuracy and convergence speed, meeting the requirements of vehicle stability.
ZHAO Shirong , SUN Yunqiang , SHI Xiling . Attitude Estimation of Octorotor Aircraft Based on Information Fusion[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2016 , 36(2) : 167 -170 . DOI: 10.15892/j.cnki.djzdxb.2016.02.041
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