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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| Main Authors: | , |
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| Format: | Conference or Workshop Item |
| Language: | English |
| Published: |
2009
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/14945/1/Integrated_Attitude_Determination.pdf http://irep.iium.edu.my/14945/ http://www.wseas.us/e-library/conferences/2009/istanbul/ACMOS/ACMOS-38.pdf |
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