SATELLITE ATTITUDE CONTROL USING DISSIMILAR REDUNDANT ACTUATORS

Date

2009-02-12

Author

Kahraman, Ozgur
Tekinalp, Ozan

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Low Earth orbit satellites are usually equipped with magnetic torquers for momentum dumping and reaction wheels to carry out three axis attitude stabilization and control. These two different types of actuators mixed and used together to carry out slew maneuvers. The problem of allocating the control to these different types of actuators is realized using a recently developed algorithm called blended inverse. The algorithm is compared with the Moore-Penrose pseudo inverse demonstrating its success in realizing the desired maneuver while overcoming singularities.

URI

https://hdl.handle.net/11511/53318

Conference Name

AAS/AIAA 19th Space Flight Mechanics Meeting

Collections

Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

O. Kahraman and O. Tekinalp, “SATELLITE ATTITUDE CONTROL USING DISSIMILAR REDUNDANT ACTUATORS,” Savannah, GA, 2009, vol. 134, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/53318.