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Quaternion Feedback Control for Spacecraft by Ali Al-Mujtaba is a document available to read on EtoBox.
This document summarizes a research paper that presents a quaternion feedback attitude control law for spacecraft using a nonlinear H-infinity approach. The paper designs a nonlinear feedback controller to achieve L2 gain performance, meaning the closed-loop system attenuates disturbances. The solution involves finding a Hamilton-Jacobi function that satisfies the H-infinity criterion. The paper applies this method to the ROCSAT-3 orbit raising control problem to validate the effectiveness of the proposed a
- Author
- Ali Al-Mujtaba
- Language
- EN