Title :
Design and simulation of satellite formation flying position-keeping control method
Author :
Liu, Yanmei ; Li, Yibo ; Xi, Jianhui
Author_Institution :
Shenyang Aerosp. Univ., Shenyang, China
Abstract :
Satellite formation flying position-keeping control is researched. A simulation method based on STK and Matlab for the satellites formation position-keeping control is introduced. Relative dynamical models of formation flying were derived, and Hill equations were deduced based on the circular reference orbit. Linear-quadratic regulator was adopted to perform the formation flying position-keeping control. Simulations in MATLAB Simulink show the successful use of LQR control approach for satellite formation flying position-keeping control.
Keywords :
Earth orbit; aircraft control; artificial satellites; linear quadratic control; mathematics computing; position control; remotely operated vehicles; satellite navigation; Hill equation; MATLAB Simulink; STK based control; circular reference orbit; dynamical model; linear quadratic regulator; satellite formation flying position keeping control method; Aerodynamics; Conferences; Equations; Mathematical model; Orbits; Satellites; Space vehicles;
Conference_Titel :
Advanced Computational Intelligence (IWACI), 2010 Third International Workshop on
Conference_Location :
Suzhou, Jiangsu
Print_ISBN :
978-1-4244-6334-3
DOI :
10.1109/IWACI.2010.5585146
