Integrated attitude determination and control system via magnetic measurements and actuation only

A nonlinear control scheme using a Modified State–Dependent Riccati Equation MSDRE has been developed through a pseudo-linearization of spacecraft augmented dynamics and kinematics. The full-state knowledge, required for the control loop is provided through a generalized algorithm for spacecraft...

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Bibliographic Details
Main Authors: Mohammad Abdel Rahman, Mohammad Ibraheem, Sang-Young, Park
Format: Proceeding Paper
Language:English
Published: 2009
Subjects:
Online Access:http://irep.iium.edu.my/14945/1/Integrated_Attitude_Determination.pdf