Spacecraft attitude control: development and application of new algorithms
The main goal of the research is to collect and develop new attitude algorithms that build up the different scenarios acted by a spacecraft starting from the orbit injection phase. It is found that the attitude scenarios can be classified mainly into two categories the first is the angular momentum...
| Main Authors: | , |
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| Format: | Book |
| Language: | English |
| Published: |
LAMBERT Academic Publishing
2012
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/23041/ http://irep.iium.edu.my/23041/1/978-3-8484-0086-7_Coverpreview.pdf |
| Summary: | The main goal of the research is to collect and develop new attitude algorithms that build up the different scenarios acted by a spacecraft starting from the orbit injection phase. It is found that the attitude scenarios can be classified mainly into two categories the first is the
angular momentum management of a spacecraft and the second is the attitude maneuvers. The first category can be divided into two modes which are the detumbling mode and the momentum unloading mode. A new algorithm for estimating the angular rates has been developed. In the second category, the attitude maneuver, the research work is concluded by developing a new technique to solve the problem of the second category using neuro-fuzzy control. |
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