Publications
Work in Progress / Under Review
2. Radial Basis Function Neural Network–Based Adaptive Attitude Control with Reaction–Wheel Health Estimation PDF
1. Adaptive Controller for Simultaneous Spacecraft Attitude Tracking and Reaction Wheel Fault Detection PDF
Journal Articles
6. Roto-Translational Control of Spacecraft in Low Earth Orbit Using Environmental Forces and Torques PDF
Show BibTeX
@Article{app11104606,
AUTHOR = {Riano-Rios, Camilo and Fedele, Alberto and Bevilacqua, Riccardo},
TITLE = {Roto-Translational Control of Spacecraft in Low Earth Orbit Using Environmental Forces and Torques},
JOURNAL = {Applied Sciences},
VOLUME = {11},
YEAR = {2021},
NUMBER = {10},
ARTICLE-NUMBER = {4606},
URL = {https://www.mdpi.com/2076-3417/11/10/4606},
ISSN = {2076-3417},
DOI = {10.3390/app11104606}
}
5. Adaptive control for differential drag-based rendezvous maneuvers with an unknown target PDF
Show BibTeX
@article{RIANORIOS2021-1,
title = {Adaptive control for differential drag-based rendezvous maneuvers with an unknown target},
journal = {Acta Astronautica},
volume = {181},
pages = {733-740},
year = {2021},
issn = {0094-5765},
doi = {https://doi.org/10.1016/j.actaastro.2020.03.011},
url = {https://www.sciencedirect.com/science/article/pii/S0094576520301399},
author = {Camilo Riano-Rios and Riccardo Bevilacqua and Warren E. Dixon},
keywords = {Differential drag, Adaptive, Atmospheric density, Drag coefficient, Rendezvous, Ballistic coefficient},
abstract = {This paper presents a differential atmospheric drag-based control algorithm for rendezvous with a non-cooperative target in Low Earth Orbit. The challenge of using a differential input that requires knowledge of physical parameters of the involved spacecraft, is addressed by designing a Lyapunov-based adaptive controller that compensates for the uncertain ballistic coefficient of the target spacecraft as well as the time-varying atmospheric density and velocity of the spacecraft relative to the atmosphere. Numerical simulations using the Schweighart-Sedwick relative dynamics are presented to validate the controller design. Additionally, simulations with more accurate dynamics for each spacecraft along with the NRLMSISE-00 model of atmospheric density are presented to evaluate the performance of the controller under nonlinearities and input saturation.}
}
4. The Drag Maneuvering Device for the SemiPassive Three-Axis Attitude Stabilization of Low Earth Orbit Nanosatellites PDF
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@article{Omar2021-1,
title = {The Drag Maneuvering Device for the SemiPassive Three-Axis Attitude Stabilization of Low Earth Orbit Nanosatellites},
journal = {Journal of Small Satellites},
volume = {10},
pages = {943-957},
year = {2021},
issn = {2327-4123},
doi = {},
url = {https://jossonline.com/wp-content/uploads/2021/03/Final-Omar-The-Drag-Maneuvering-Device-for-the-Semi-Passive-Three-Axis-Attitude-Stabilization-of-Low-Earth-Orbit-Nanosatellites.pdf},
author = {Sanny Omar and Camilo Riano-Rios and Riccardo Bevilacqua},
keywords = {},
}
3. Aerodynamic and gravity gradient based attitude control for CubeSats in the presence of environmental and spacecraft uncertainties PDF
Show BibTeX
@article{RIANORIOS2021,
title = {Aerodynamic and gravity gradient based attitude control for CubeSats in the presence of environmental and spacecraft uncertainties},
journal = {Acta Astronautica},
volume = {180},
pages = {439-450},
year = {2021},
issn = {0094-5765},
doi = {https://doi.org/10.1016/j.actaastro.2020.12.038},
url = {https://www.sciencedirect.com/science/article/pii/S0094576520307724},
author = {Camilo Riano-Rios and Runhan Sun and Riccardo Bevilacqua and Warren E. Dixon},
keywords = {Aerodynamic torque, Gravity gradient torque, Atmospheric density, Drag, Lift, Center of mass, Adaptive},
}
2. CubeSat Adaptive Attitude Control with Uncertain Drag Coefficient and Atmospheric Density PDF
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@article{Sun2021,
author = {Sun, Runhan and Riano-Rios, Camilo and Bevilacqua, Riccardo and Fitz-Coy, Norman G. and Dixon, Warren E.},
title = {CubeSat Adaptive Attitude Control with Uncertain Drag Coefficient and Atmospheric Density},
journal = {Journal of Guidance, Control, and Dynamics},
volume = {44},
number = {2},
pages = {379-388},
year = {2021},
doi = {10.2514/1.G005515},
URL = {https://doi.org/10.2514/1.G005515},
eprint = {https://doi.org/10.2514/1.G005515}
}
1. Differential drag-based multiple spacecraft maneuvering and on-line parameter estimation using integral concurrent learning PDF
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@article{RIANORIOS2020,
title = {Differential drag-based multiple spacecraft maneuvering and on-line parameter estimation using integral concurrent learning},
journal = {Acta Astronautica},
volume = {174},
pages = {189-203},
year = {2020},
issn = {0094-5765},
doi = {https://doi.org/10.1016/j.actaastro.2020.04.059},
url = {https://www.sciencedirect.com/science/article/pii/S0094576520302745},
author = {Camilo Riano-Rios and Riccardo Bevilacqua and Warren E. Dixon},
keywords = {Differential drag, Adaptive, Atmospheric density, Drag coefficient, Rendezvous, Formation, Integral concurrent learning}
}
Conference Papers
9. Real-Time Estimation of Drag-Based Parameters in LEO via Adaptive Control and Sparse Identification PDF
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@inbook{doi:10.2514/6.2026-2625,
author = {Morokot Sakal and Camilo Riano-Rios and Madhur Tiwari},
title = {Real-Time Estimation of Drag-Based Parameters in LEO via Adaptive Control and Sparse Identification},
booktitle = {AIAA SCITECH 2026 Forum},
chapter = {},
pages = {},
doi = {10.2514/6.2026-2625},
URL = {https://arc.aiaa.org/doi/abs/10.2514/6.2026-2625},
eprint = {https://arc.aiaa.org/doi/pdf/10.2514/6.2026-2625}
}
8. Real-Time Testing of Satellite Attitude Control with A Reaction Wheel Hardware-In-the-Loop Platform PDF
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@inproceedings{2025sakal-2,
title = {Real-Time Testing of Satellite Attitude Control with A Reaction Wheel Hardware-In-the-Loop Platform},
author = {Sakal, Morokot and Nehma, George and Riano-Rios, Camilo and Tiwari, Madhur},
booktitle = {Proceedings of the 2025 AAS/AIAA Astrodynamics Specialist Conference},
year = {2025},
address = {Boston, MA, USA},
note = {Paper AAS 25-778}
}
7. RBFNN-based Adaptive Attitude Controller with Reaction Wheel Health Estimation PDF
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@inproceedings{2025sakal-1,
title = {RBFNN-based Adaptive Attitude Controller with Reaction Wheel Health Estimation},
author = {Sakal, Morokot and Nehma, George and Riano-Rios, Camilo and Tiwari, Madhur},
booktitle = {Proceedings of the 2025 AAS/AIAA Astrodynamics Specialist Conference},
year = {2025},
address = {Boston, MA, USA},
note = {Paper AAS 25-682}
}
6. Adaptive controller for simultaneous spacecraft attitude tracking and reaction wheel fault detection PDF
Show BibTeX
@inproceedings{2024rianorios,
title = {Adaptive controller for simultaneous spacecraft attitude tracking and reaction wheel fault detection},
author = {Riano-Rios, Camilo and Nehma, George and Tiwari, Madhur},
booktitle = {Proceedings of the 2024 AAS/AIAA Astrodynamics Specialist Conference},
year = {2024},
address = {Broomfield, CO, USA},
note = {Paper AAS 22-440}
}
5. Simultaneous Attitude Control and Modes Estimation for Flexible Spacecraft using Adaptive Control and Integral Concurrent Learning PDF
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@InProceedings{10.1007/978-3-031-51928-4_42,
author="Bevilacqua, R.
and Riano-Rios, C.
and Sinclair, A.",
editor="Sandnas, Matt
and Spencer, David B.",
title="SIMULTANEOUS ATTITUDE CONTROL AND MODES ESTIMATION FOR FLEXIBLE SPACECRAFT USING ADAPTIVE CONTROL AND INTEGRAL CONCURRENT LEARNING",
booktitle="Proceedings of the 44th Annual American Astronautical Society Guidance, Navigation, and Control Conference, 2022",
year="2024",
publisher="Springer International Publishing",
address="Cham",
pages="717--730",
isbn="978-3-031-51928-4"
}
4. Approximate Optimal Orbit Transfer of Non-cooperative Debris PDF
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@inbook{doi:10.2514/6.2020-1823,
author = {Max L. Greene and Camilo Riano-Rios and Riccardo Bevilacqua and Norman G. Fitz-Coy and Warren Dixon},
title = {Approximate Optimal Orbit Transfer of Non-cooperative Debris},
booktitle = {AIAA Scitech 2020 Forum},
chapter = {},
pages = {},
doi = {10.2514/6.2020-1823},
URL = {https://arc.aiaa.org/doi/abs/10.2514/6.2020-1823},
eprint = {https://arc.aiaa.org/doi/pdf/10.2514/6.2020-1823}
}
3. Spacecraft Attitude Regulation in Low Earth Orbit Using Natural Torques PDF
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@inproceedings{2019rianorios,
title = {Spacecraft Attitude Regulation in Low Earth Orbit Using Natural Torques},
author = {Riano-Rios, Camilo and Omar, Sanny and Bevilacqua, Riccardo and Dixon, Warren},
booktitle = {Proceedings of the 4th IEEE Colombian Conference on Automatic Control CCAC},
year = {2019},
address = {Medellin, Colombia},
note = {}
}
2. Semi-Passive Three Axis Attitude Stabilization for Earth Observation Satellites using the Drag Maneuvering Device PDF
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@inproceedings{2019omar,
title = {Semi-Passive Three Axis Attitude Stabilization for Earth Observation Satellites using the Drag Maneuvering Device},
author = {Omar, Sanny and Riano-Rios, Camilo and Bevilacqua, Riccardo},
booktitle = {12th IAA Symposium on Small Satellite for Earth Observation},
year = {2019},
address = {Berlin, Germany},
note = {}
}
1. Relative Maneuvering for Multiple Spacecraft Via Differential Drag Using LQR and Constrained Least Squares PDF
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@inproceedings{2019rianorios,
title = {Relative Maneuvering for Multiple Spacecraft Via Differential Drag Using LQR and Constrained Least Squares},
author = {Riano-Rios, Camilo and Bevilacqua, Riccardo and Dixon, Warren},
booktitle = {Proceedings of the AAS/AIAA Space Flight Mechanics Meeting},
year = {2019},
address = {Ka’anapali, HI, USA},
note = {Paper AAS 19-346}
}
