Spacecraft attitude control via a combined state-dependent Riccati equation and adaptive neuro-fuzzy approach
A hybrid nonlinear controller for spacecraft attitude and rate tracking is presented though a combination of two control techniques. Based on the augmentation of spacecraft dynamics and kinematics, a pseudo-linear formulation is derived and used for the development of the basic controller. The bas...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Elsevier Masson SAS
2011
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/8584/ http://irep.iium.edu.my/8584/ http://irep.iium.edu.my/8584/4/AST_Revised_2_.pdf |