@inproceedings{44686f760b694b93ba0ffc2acbff3ae8,
title = "Spacecraft attitude control using approximate receding-horizon model-error control synthesis",
abstract = "Model-error control synthesis is a nonlinear robust control approach that mitigates the effects of modeling errors and disturbances on a system by providing corrections to the nominal control input directly. In this paper model-error control synthesis is applied to the spacecraft attitude control problem, where the model-error vector is computed using a receding-horizon approximation. The main advantage of this approach over other adaptive approaches for spacecraft attitude control is that it can simultaneously handle both inertia modeling errors and time varying disturbances. A design scheme is presented to determine the weighting factor and the length of the associated receding-horizon interval of the model-error solution by minimizing the closed-loop sensitivity norm. Simulation results are provided to show the performance of the new control approach.",
author = "Jongrae Kim and Crassidis, \{John L.\}",
year = "2005",
doi = "10.2514/6.2005-6178",
language = "English",
isbn = "1563477378",
series = "Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
pages = "3359--3373",
booktitle = "Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2005",
note = "AIAA Guidance, Navigation, and Control Conference 2005 ; Conference date: 15-08-2005 Through 18-08-2005",
}