T.S.C. Pollack

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13 Conference contribution
3 Article
3 Conference article
1 Dissertation (TU Delft)

Duality Between Incremental Nonlinear Dynamic Inversion and Quasi-Linear Parameter-Varying Control
Pollack, T. S. C., Theodoulis, S. & Wang, X., 2026, (E-pub ahead of print) In: Journal of Guidance, Control, and Dynamics: devoted to the technology of dynamics and control. 17 p.
Research output: Contribution to journal › Article › Scientific › peer-review

Open Access
Duality Between Incremental Nonlinear Dynamic Inversion and Transformation-Based Quasi-Linear Parameter-Varying Control
Pollack, T. S. C., Theodoulis, S. & Wang, X., 2026, Proceedings of the AIAA SCITECH 2026 Forum. American Institute of Aeronautics and Astronautics Inc. (AIAA), 25 p. AIAA 2026-0108. (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026).
Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

Open Access
File
8 Downloads (Pure)
Multi-Objective Synthesis of Hybrid Incremental Dynamic Inversion Control Laws Using H _∞ Loop-Shaping
Silva Encarnação, L., Pollack, T. S. C., Looye, G. H. N. & Theodoulis, S., 2026, Proceedings of the AIAA SCITECH 2026 Forum. American Institute of Aeronautics and Astronautics Inc. (AIAA), 25 p. AIAA 2026-0551. (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026).
Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

Open Access
File
3 Downloads (Pure)
Robust Control Design for the Flying V Aircraft within the Signal-Based H _∞Framework
Pedroso, B., Pollack, T. S. C. & Theodoulis, S., 2026, Proceedings of the AIAA SCITECH 2026 Forum. American Institute of Aeronautics and Astronautics Inc. (AIAA), 25 p. AIAA 2026-1952. (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2026).
Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

Open Access
File
5 Downloads (Pure)
Quasi-LPV Transformations for Robust Gain Scheduling of Incremental Nonlinear Dynamic Inversion-based Controllers
Pollack, T., Theodoulis, S. & Wang, X., 2025, In: IFAC-PapersOnline. 59, 15, p. 97-102 6 p.
Research output: Contribution to journal › Conference article › Scientific › peer-review

Open Access
File
2 Link opens in a new tab Citations (Scopus)

2 Downloads (Pure)

MATLAB/SIMULINK(R) Code and Supporting Data for Design of Multi-objective Incremental Control Allocation-based Flight Control Laws
Pollack, T. (Creator), TU Delft - 4TU.ResearchData, 8 Oct 2024
DOI: 10.4121/B265AE09-64EF-4FAF-BD77-D18712C11239
Dataset/Software: Dataset
MATLAB/SIMULINK(R) Code and Supporting Data for Analysis of Inversion Strategy on Robustness of IDI-based Control Laws
Pollack, T. (Creator), TU Delft - 4TU.ResearchData, 8 Oct 2024
DOI: 10.4121/1C3B2FE8-15EE-4C93-9DE3-9E5DDDACA6A0
Dataset/Software: Dataset
MATLAB/SIMULINK(R) Code and Supporting Data for Multi-loop Robust Design of INDI-based Flight Control Laws
Pollack, T. (Creator), TU Delft - 4TU.ResearchData, 8 Oct 2024
DOI: 10.4121/4A2AFA5B-CC72-4EBE-ADCA-970E2FC0D988
Dataset/Software: Dataset
MATLAB/SIMULINK(R) Code and Supporting Data for Assessment of Commonalities between Hybrid INDI-based and PID-based Flight Control Design
Pollack, T. (Creator), TU Delft - 4TU.ResearchData, 8 Oct 2024
DOI: 10.4121/1C425F5D-943C-4E9C-8C6B-4E026DBA20CA
Dataset/Software: Dataset

T.S.C. Pollack

Fingerprint

Collaborations and top research areas from the last five years

Dive into details

Duality Between Incremental Nonlinear Dynamic Inversion and Quasi-Linear Parameter-Varying Control

Duality Between Incremental Nonlinear Dynamic Inversion and Transformation-Based Quasi-Linear Parameter-Varying Control

Multi-Objective Synthesis of Hybrid Incremental Dynamic Inversion Control Laws Using H _∞ Loop-Shaping

Robust Control Design for the Flying V Aircraft within the Signal-Based H _∞Framework

Quasi-LPV Transformations for Robust Gain Scheduling of Incremental Nonlinear Dynamic Inversion-based Controllers

MATLAB/SIMULINK(R) Code and Supporting Data for Design of Multi-objective Incremental Control Allocation-based Flight Control Laws

MATLAB/SIMULINK(R) Code and Supporting Data for Analysis of Inversion Strategy on Robustness of IDI-based Control Laws

MATLAB/SIMULINK(R) Code and Supporting Data for Multi-loop Robust Design of INDI-based Flight Control Laws

MATLAB/SIMULINK(R) Code and Supporting Data for Assessment of Commonalities between Hybrid INDI-based and PID-based Flight Control Design

T.S.C. Pollack

Fingerprint

Collaborations and top research areas from the last five years

Research output

Datasets