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Spacecraft Attitude Maneuver Control Using Linear Model Following Nonlinear Adaptive Controller

Published in Korean (English title shown)

Jihoon Lee, Suwon Lee, Byunghoon Kim, Youdan Kim, Gwanghyeok Ju

2016 KSAS Spring Conference (KSAS 2016S), Goseong, Korea, Apr. 2016

Fig. 4. Control Inputs
Fig. 4. Control Inputs
Fig. 2. Angular rates in detumbling
Fig. 2. Angular rates in detumbling

Figures and captions reproduced from the paper (© the authors and original publisher).

Attitude control is essential for spacecraft mission. In this study, linear model following nonlinear adaptive controller is expanded so that it could be applied to spacecraft attitude maneuvers. Numerical simulations under actuator saturation demonstrate that the designed controller meets performance objectives in the presence of actuator saturation and uncertainties.

DBpiahttps://www.dbpia.co.kr/journal/articleDetail?nodeId=NODE07068013BibTeX@inproceedings{Lee2016, title = {Spacecraft Attitude Maneuver Control Using Linear Model Following Nonlinear Adaptive Controller}, author = {Jihoon Lee and Suwon Lee and Byunghoon Kim and Youdan Kim and Gwanghyeok Ju}, year = {2016}, booktitle = {2016 KSAS Spring Conference (KSAS 2016S), Goseong, Korea, Apr. 2016}, note = {Original Korean title: 선형모델 추종 비선형 적응제어기를 이용한 인공위성 자세기동}, }

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