Multi-Object Attitude and Rate Tracking for Spacecraft in Formation Flying

This paper presents the application of a Modified State–Dependent Riccati Equation MSDRE approach in multi-object attitude and rate tracking. A nonlinear controller using the MSDRE is developed through a pseudo-linearization of spacecraft augmented nonlinear absolute dynamics and kinematics. The de...

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Bibliographic Details
Main Author: Mohammad Abdelrahman, Mohammad Ibraheem
Format: Conference or Workshop Item
Language:English
Published: 2011
Subjects:
Online Access:http://irep.iium.edu.my/7304/
http://irep.iium.edu.my/7304/1/AIAA-2011-6236-978.pdf