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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| Format: | Conference or Workshop Item |
| Language: | English |
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2011
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| Online Access: | http://irep.iium.edu.my/7304/ http://irep.iium.edu.my/7304/1/AIAA-2011-6236-978.pdf |