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Slew Maneuver Control of Flexible Spacecraft
Date
2019-07-04
Author
ALTINIŞIK, SÜLEYMAN
Tekinalp, Ozan
Metadata
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This work is licensed under a
Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
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Nonlinear slew maneuver algorithms for flexible spacecraft are developed. Theattitude trackingalgorithm that uses quaternion parametrizationand follows the prescribed time dependent attitude trajectory incorporating the derivative of the desired attitudeis employed. Nonlinear tracking feedback control algorithms that includes piezoelectric actuators and modal sensors are also developed. Through simulations, the effectiveness of the tracking attitude control algorithm is demonstrated. Also demonstrated is the effectiveness of the tracking controller utilizing piezoelectric actuators modal sensors in damping out vibration energy.
URI
https://hdl.handle.net/11511/58049
DOI
https://doi.org/10.13009/eucass2019-935
Collections
Department of Aerospace Engineering, Conference / Seminar