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Thomas Lombaerts
Thomas Lombaerts
Senior Aerospace Research Engineer at NASA Ames Research Center
Verified email at nasa.gov
Title
Cited by
Cited by
Year
Fault tolerant flight control
C Edwards, T Lombaerts, H Smaili
Lecture notes in control and information sciences 399, 1-560, 2010
3912010
Nonlinear reconfiguring flight control based on online physical model identification
TJJ Lombaerts, HO Huisman, QP Chu, JA Mulder, DA Joosten
Journal of Guidance, Control, and Dynamics 32 (3), 727-748, 2009
842009
Online aerodynamic model structure selection and parameter estimation for fault tolerant control
TJJ Lombaerts, ER Van Oort, QP Chu, JA Mulder, DA Joosten
Journal of guidance, control, and dynamics 33 (3), 707-723, 2010
662010
Dynamic inversion based full envelope flight control for an eVTOL vehicle using a unified framework
T Lombaerts, J Kaneshige, S Schuet, BL Aponso, KH Shish, G Hardy
AIAA Scitech 2020 Forum, 1619, 2020
602020
A simulation benchmark for integrated fault tolerant flight control evaluation
H Smaili, J Breeman, T Lombaerts, D Joosten
AIAA modeling and simulation technologies conference and exhibit, 6471, 2006
592006
Safe maneuvering envelope estimation based on a physical approach
T Lombaerts, S Schuet, K Wheeler, DM Acosta, J Kaneshige
Aiaa guidance, navigation, and control (gnc) conference, 4618, 2013
582013
Effects of structural failure on the safe flight envelope of aircraft
HN Nabi, T Lombaerts, Y Zhang, E Van Kampen, QP Chu, CC de Visser
Journal of Guidance, Control, and Dynamics 41 (6), 1257-1275, 2018
562018
Fault tolerant flight control, a physical model approach
T Lombaerts, P Chu, JAB Mulder, O Stroosma
Advances in Flight Control Systems, 2011
552011
Nonlinear dynamic inversion based attitude control for a hovering quad tiltrotor eVTOL vehicle
T Lombaerts, J Kaneshige, S Schuet, G Hardy, BL Aponso, KH Shish
AIAA Scitech 2019 forum, 0134, 2019
532019
Control concepts for simplified vehicle operations of a quadrotor eVTOL vehicle
T Lombaerts, J Kaneshige, M Feary
AIAA aviation 2020 forum, 3189, 2020
432020
Design and piloted simulator evaluation of adaptive safe flight envelope protection algorithm
T Lombaerts, G Looye, J Ellerbroek, MR Martin
Journal of Guidance, Control, and Dynamics 40 (8), 1902-1924, 2017
422017
Piloted simulator evaluation results of new fault-tolerant flight control algorithm
TJJ Lombaerts, MH Smaili, O Stroosma, QP Chu, JA Mulder, DA Joosten
Journal of Guidance, Control, and Dynamics 32 (6), 1747-1765, 2009
422009
Autonomous flight envelope estimation for loss-of-control prevention
S Schuet, T Lombaerts, D Acosta, J Kaneshige, K Wheeler, K Shish
Journal of Guidance, Control, and Dynamics 40 (4), 847-862, 2017
382017
Pseudo control hedging and its application for safe flight envelope protection
T Lombaerts, G Looye, P Chu, JA Mulder
AIAA Guidance, Navigation, and Control Conference, 8280, 2010
352010
Modular flight control reconfiguration design and simulation
TJJ Lombaerts, QP Chu, JA Mulder, DA Joosten
Control Engineering Practice 19 (6), 540-554, 2011
342011
An adaptive nonlinear aircraft maneuvering envelope estimation approach for online applications
S Schuet, T Lombaerts, D Acosta, K Wheeler, J Kaneshige
Aiaa guidance, navigation, and control conference, 0268, 2014
332014
Piloted simulator evaluation of safe flight envelope display indicators for loss of control avoidance
T Lombaerts, S Schuet, D Acosta, J Kaneshige, K Shish, L Martin
Journal of Guidance, Control, and Dynamics 40 (4), 948-963, 2017
322017
On-line safe flight envelope determination for impaired aircraft
T Lombaerts, S Schuet, D Acosta, J Kaneshige
Advances in Aerospace Guidance, Navigation and Control: Selected Papers of …, 2015
302015
Trajectory Prediction and Alerting for Aircraft Mode and Energy State Awareness
K Shish, J Kaneshige, D Acosta, S Schuet, T Lombaerts, L Martin, ...
AIAA Infotech @ Aerospace, 2015
292015
Design and simulation of fault tolerant flight control based on a physical approach
TJJ Lombaerts, GHN Looye, QP Chu, JA Mulder
Aerospace Science and Technology 23 (1), 151-171, 2012
292012
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