| Design of Dynamic Inversion and Explicit Model Following Flight Control Laws for Quadrotor UAS U Saetti, J Horn, S Lajhmani, C Lagoa, T Berger Journal of the American Helicopter Society 65 (032006), 2020 | 19 | 2020 |
| Rotorcraft simulations with coupled flight dynamics, free wake, and acoustics U Saetti | 18 | 2016 |
| Use of Harmonic Decomposition Models in Rotorcraft Flight Control Design with Alleviation of Vibratory Loads U Saetti, J Horn European Rotorcraft Forum 2017, 2017 | 13 | 2017 |
| Tools for Development and Analysis of Rotorcraft Noise Abatement Y Li, K Brentner, K Sharma, J Horn, U Saetti Sustainability 2015, Montreal, Quebec, Canada, 2015 | 11 | 2015 |
| Revisited Harmonic Balance Trim Solution Method for Periodically-Forced Aerospace Vehicles U Saetti, J Rogers Journal of Guidance, Control, and Dynamics, 2021 | 10 | 2021 |
| Handling-Qualities Perspective on Rotorcraft Load Alleviation Control U Saetti, J Horn, T Berger, M Tischler Journal of Guidance, Control, and Dynamics, 2020 | 10 | 2020 |
| Identification of linear time-periodic systems from rotorcraft flight-test data U Saetti, JF Horn, T Berger, MJS Lopez, MB Tischler Journal of Guidance, Control, and Dynamics 42 (10), 2288-2296, 2019 | 10 | 2019 |
| Load Alleviation Flight Control Design using High-Order Dynamic Models U Saetti, J Horn Journal of the American Helicopter Society 65 (032006), 2020 | 9 | 2020 |
| Helicopter Simulations with Coupled Flight Dynamics, Free Wake, and Acoustics U Saetti, W Villafana, DA Wachspress, KS Brentner, JF Horn AHS International 72nd Annual Forum Proceedings, 16-19, 2016 | 8 | 2016 |
| Harmonic Decomposition Models of Flapping-Wing Flight for Stability Analysis and Control Design U Saetti, J Rogers Journal of Guidance, Control, and Dynamics, 2022 | 7 | 2022 |
| Load Alleviation Control using Dynamic Inversion with Direct Load Feedback M Scaramal, JF Horn, U Saetti Vertical Flight Society Forum 77, 2021 | 7 | 2021 |
| Load Alleviation Control Design Using Harmonic Decomposition Models, Rotor State Feedback, and Redundant Control Effectors U Saetti, JF Horn | 7 | 2018 |
| Flight Dynamics and Control of an eVTOL Concept Aircraft with a Propeller-Driven Rotor U Saetti, J Enciu, J Horn Journal of the American Helicopter Society 67, 1-14(14), 2022 | 6 | 2022 |
| Performance and Design Optimization of the F-Helix eVTOL Concept U Saetti, J Enciu, J Horn Vertical Flight Society Forum 75, 2019 | 6 | 2019 |
| Rotorcraft Flight Control Design with Alleviation of Unsteady Rotor Loads U Saetti, J Horn, T Berger, M Tischler Vertical Flight Society Forum 75, 2019 | 5 | 2019 |
| Tiltrotor simulations with coupled flight dynamics, state-space aeromechanics, and aeroacoustics U Saetti, B Buğday Journal of the American Helicopter Society 69 (1), 1-18, 2024 | 4 | 2024 |
| Implementation and Linearization of a Rotor Simulation with a State-Space Free-Vortex Wake Model U Saetti, J Horn Vertical Flight Society Forum 78, 2022 | 4 | 2022 |
| Implementation and Linearization of a State-Space Free-Vortex Wake Model for Flapping-Wing Flight U Saetti, J Horn Vertival Flight Society Forum 78, 2022 | 3 | 2022 |
| Flight Simulation and Control using the Julia Language U Saetti, Horn, Joseph 2022 AIAA SciTech Forum, 2022 | 3 | 2022 |
| Time-Periodic and High-Order Time-Invariant Linearized Models of Rotorcraft: A Survey U Saetti, M Lovera Journal of the American Helicopter Society 67 (4), 1-9, 2021 | 3 | 2021 |
Tom BergerResearch Engineer, U.S. Army Aviation Development Directorate, AMRDECVerified email at mail.mil
