A Total Energy Attitude Control System Strategy for Rigid Spacecraft

A Total Energy Attitude Control System Strategy for Rigid Spacecraft

This paper aims to design a controller based on the Total Energy Control System (TECS) method, to solve the attitude trajectory tracking problem for rigid spacecraft. TECS objective is to command the total energy rate using a proportional-integral (PI) controller. The attitude control objective fixe...

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Bibliographic Details
Main Authors: Rolando Cortes-Martinez, Hugo Rodriguez-Cortes
Format: Article
Language:English
Published: IEEE 2019-01-01
Series:IEEE Access
Subjects:
Attitude control
Hamiltonian dynamics
Lyapunov theory
real-time control
Online Access:https://ieeexplore.ieee.org/document/8794491/

Internet

https://ieeexplore.ieee.org/document/8794491/

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