z-logo
open-access-imgOpen Access
Design of an Adaptive Controller of a Satellite using Thruster Actuator
Author(s) -
Alireza Fazlyab,
Abbas Ajorkar,
Mansour Kabganian
Publication year - 2014
Publication title -
international journal of computer applications
Language(s) - English
Resource type - Journals
ISSN - 0975-8887
DOI - 10.5120/17849-8798
Subject(s) - computer science , actuator , satellite , controller (irrigation) , aerospace engineering , simulation , aeronautics , artificial intelligence , engineering , agronomy , biology
this paper, an attitude control algorithm for a satellite is developed based on adaptive control using thruster actuators. For this purpose a twelve-thruster arrangement has been considered and the control torque for each thruster has been calculated. Then a Pulse Width-Pulse Frequency (PWPF) modulator is used for converting continuous controller signals into equivalent discrete one. Then, uncertainties in the moment of inertia matrix and disturbances torque has been considered and adaptive attitude control using feedback linearization controller with self-tuning regulator (Least Square Estimator With Bounded Gain Factor) is used. Finally, the performance of the designed attitude controller is investigated by simulations. KeywordsControl; Adaptive control; Satellite; Reaction

The content you want is available to Zendy users.

Already have an account? Click here to sign in.
Having issues? You can contact us here
Accelerating Research

Address

John Eccles House
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom