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Raghu Venkataraman
Raghu Venkataraman
Research Scientist, Amazon
Bestätigte E-Mail-Adresse bei umn.edu
Titel
Zitiert von
Zitiert von
Jahr
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
282019
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
222014
Reliability assessment of actuator architectures for unmanned aircraft
R Venkataraman, P Seiler, M Lukátsi, B Vanek
Journal of Aircraft 54 (3), 955-966, 2017
212017
System identification for a small, rudderless, fixed-wing unmanned aircraft
R Venkataraman, P Seiler
Journal of Aircraft 56 (3), 1126-1134, 2019
192019
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
182018
Reliability Assessment of Actuator Architectures for Unmanned Aircraft
R Venkataraman
University of Minnesota, 2015
132015
Reliability Assessment of Actuator Architectures for Unmanned Aircraft
R Venkataraman, M Lukátsi, B Vanek, P Seiler
IFAC-PapersOnLine 48 (21), 398-403, 2015
132015
Fault-tolerant flight control using one aerodynamic control surface
R Venkataraman, P Seiler
Journal of Guidance, Control, and Dynamics 42 (3), 570-584, 2019
122019
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
122015
Robust LPV estimator synthesis using integral quadratic constraints
R Venkataraman, P Seiler
2016 American Control Conference (ACC), 4611-4616, 2016
102016
Fault-tolerant aircraft flight control using a subset of aerodynamic control surfaces
R Venkataraman, P Seiler, B Taylor
US Patent 10,604,236, 2020
92020
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
92017
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
72016
Safe flight using one aerodynamic control surface
R Venkataraman, P Seiler
AIAA Science and Technology Forum and Exposition, Paper No. AIAA 2016-0634, 2016
62016
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
52017
Trajectory‐based robustness analysis for nonlinear systems
P Seiler, R Venkataraman
International Journal of Robust and Nonlinear Control 34 (2), 910-926, 2024
2024
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
2023
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
Vireo Flight 33
R Venkataraman
2017
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