| Comparison of fault detection and isolation methods for a small unmanned aircraft R Venkataraman, P Bauer, P Seiler, B Vanek Control Engineering Practice 84, 365-376, 2019 | 36 | 2019 |
| Reliability Assessment of Actuator Architectures for Unmanned Aircraft R Venkataraman, M Lukátsi, B Vanek, P Seiler IFAC-PapersOnLine 48 (21), 398-403, 2015 | 29 | 2015 |
| Fault detection and basic in-flight reconfiguration of a small uav equipped with elevons P Bauer, R Venkataraman, B Vanek, PJ Seiler, J Bokor IFAC-PapersOnLine 51 (24), 600-607, 2018 | 22 | 2018 |
| Formation flying with nonlinear partial integrated guidance and control R Padhi, PR Rakesh, R Venkataraman IEEE Transactions on Aerospace and Electronic Systems 50 (4), 2847-2859, 2014 | 22 | 2014 |
| System identification for a small, rudderless, fixed-wing unmanned aircraft R Venkataraman, P Seiler Journal of Aircraft 56 (3), 1126-1134, 2019 | 20 | 2019 |
| Reliability Assessment of Actuator Architectures for Unmanned Aircraft R Venkataraman University of Minnesota, 2015 | 17 | 2015 |
| Convex LPV synthesis of estimators and feedforwards using duality and integral quadratic constraints R Venkataraman, P Seiler International Journal of Robust and Nonlinear Control 28 (3), 953-975, 2017 | 14 | 2017 |
| Fault-tolerant flight control using one aerodynamic control surface R Venkataraman, P Seiler Journal of Guidance, Control, and Dynamics 42 (3), 570-584, 2019 | 12 | 2019 |
| Model-Based Detection and Isolation of Rudder Faults for a Small UAS R Venkataraman, PJ Seiler AIAA Science and Technology Forum and Exposition, Paper No. AIAA 2015-0857, 2015 | 12 | 2015 |
| Quantifying Loss-of-Control Envelopes via Robust Tracking Analysis H Pfifer, R Venkataraman, P Seiler Journal of Guidance, Control, and Dynamics 40 (4), 1042-1050, 2016 | 10 | 2016 |
| Robust LPV estimator synthesis using integral quadratic constraints R Venkataraman, P Seiler 2016 American Control Conference (ACC), 4611-4616, 2016 | 10 | 2016 |
| Fault-tolerant aircraft flight control using a subset of aerodynamic control surfaces R Venkataraman, P Seiler, B Taylor US Patent 10,604,236, 2020 | 9 | 2020 |
| Comparison of Fault-Tree Models for Fault Detection, Isolation, and Recovery Algorithms TJ Leung, JH Rife, P Seiler, R Venkataraman Journal of Aerospace Information Systems 14 (9), 517-522, 2017 | 6 | 2017 |
| Safe flight using one aerodynamic control surface R Venkataraman, P Seiler AIAA Science and Technology Forum and Exposition, Paper No. AIAA 2016-0634, 2016 | 6 | 2016 |
| Assessment of metrics that measure the effectiveness of control allocation and their use in linear closed-loop analysis U Zalluhoglu, R Venkataraman, M Ceze, H Carson, M Szmuk, ... AIAA SciTech 2023 Forum, 1052, 2023 | 2 | 2023 |
| Vireo Flight 29 R Venkataraman | 1 | 2017 |
| Trajectory‐based robustness analysis for nonlinear systems P Seiler, R Venkataraman International Journal of Robust and Nonlinear Control 34 (2), 910-926, 2024 | | 2024 |
| Comparison of Methods to Verify Probabilistic Aerospace Requirements S Bhan, R Venkataraman, B Novak, S Airoldi, C McFarland AIAA SCITECH 2023 Forum, 1480, 2023 | | 2023 |
| Research Overview J Hoyt, P Singh, W Energy, R Venkataraman, A Gupta, C Regan, C Olson, ... | | 2018 |
| Designing Reliability Into Small UAS Avionics: Part 2 I Lakshminarayan, R Venkataraman, D Ossmann, P Seiler, ... Inside Unmanned Systems Magazine, 54-57, 2016 | | 2016 |
Peter Seiler JrUniversity of Michigan, Ann ArborBestätigte E-Mail-Adresse bei umich.edu
