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Nicolas Bérend
Nicolas Bérend
ONERA - The French Aerospace Lab
Verified email at onera.fr
Title
Cited by
Cited by
Year
A survey of multidisciplinary design optimization methods in launch vehicle design
M Balesdent, N Bérend, P Dépincé, A Chriette
Structural and Multidisciplinary optimization 45, 619-642, 2012
1642012
Interior-point approach to trajectory optimization
J Laurent-Varin, JF Bonnans, N Bérend, M Haddou, C Talbot
Journal of Guidance, Control, and Dynamics 30 (5), 1228-1238, 2007
762007
Bi-objective optimization of a multiple-target active debris removal mission
N Bérend, X Olive
Acta Astronautica 122, 324-335, 2016
592016
Estimation of the probability of collision between two catalogued orbiting objects
N Bérend
Advances in Space Research 23 (1), 243-247, 1999
551999
Overview of some optimal control methods adapted to expendable and reusable launch vehicle trajectories
N Berend, C Talbot
Aerospace science and technology 10 (3), 222-232, 2006
382006
Decoupled multidisciplinary design optimization formulation for interdisciplinary coupling satisfaction under uncertainty
L Brevault, M Balesdent, N Bérend, R Le Riche
AIAA Journal 54 (1), 186-205, 2016
322016
Stagewise multidisciplinary design optimization formulation for optimal design of expendable launch vehicles
M Balesdent, N Bérend, P Dépincé
Journal of Spacecraft and Rockets 49 (4), 720-730, 2012
312012
Multidisciplinary Aerospace System Design: Principles, Issues and Onera Experience.
S Defoort, M Balesdent, P Klotz, P Schmollgruber, J Morio, J Hermetz, ...
Aerospace Lab, p. 1-15, 2012
262012
Comparison of different global sensitivity analysis methods for aerospace vehicle optimal design
L Brevault, M Balesdent, N Bérend, R Le Riche
10th World Congress on Structural and Multidisciplinary Optimization, WCSMO …, 2013
252013
Challenges and future trends in uncertainty-based multidisciplinary design optimization for space transportation system design
L Brevault, M Balesdent, N Bérend, R Le Riche
5th European conference for aeronautics and space sciences (EUCASS 2013), 2013
152013
Advanced space vehicle design taking into account multidisciplinary couplings and mixed epistemic/aleatory uncertainties
M Balesdent, L Brevault, NB Price, S Defoort, R Le Riche, NH Kim, ...
Space Engineering: Modeling and Optimization with Case Studies, 1-48, 2016
142016
Multi-level hierarchical MDO formulation with functional coupling satisfaction under uncertainty, application to sounding rocket design
L Brevault, M Balesdent, N Bérend, R Le Riche
World Congress on Structural and Multidisciplinary Optimization, 7-12, 2015
142015
New multidisciplinary design optimization approaches for launch vehicle design
M Balesdent, N Bérend, P Dépincé
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2013
142013
Optimization method for mission analysis of aeroassisted orbital transfer vehicles
N Bérend, S Bertrand, C Jolly
Aerospace science and technology 11 (5), 432-441, 2007
142007
On the refinement of discretization for optimal control problems
J Laurent-Varin, F Bonnans, N Berend, C Talbot, M Haddou
IFAC Proceedings Volumes 37 (6), 405-410, 2004
142004
Multidisciplinary design optimization of multi-stage launch vehicle using flight phases decomposition
M Balesdent, N Bérend, P Dépincé, A Chriette
International Journal for Simulation and Multidisciplinary Design …, 2010
122010
Optimal design of expendable launch vehicles using stage-wise MDO formulation
M Balesdent, N Bérend, P Dépincé
13th AIAA/ISSMO multidisciplinary analysis optimization conference, 9324, 2010
112010
MDO approach for early design of aerobraking orbital transfer vehicles
N Bérend, S Bertrand
Acta Astronautica 65 (11-12), 1668-1678, 2009
102009
ALTAIR Semi-Reusable Air-Launch System-Current Design and Status of Flight Experiments
N Bérend, J Gauvrit-Ledogar, F Perrel, J Oswald, E Diez, C Dupont, ...
8th European Conference for Aerospace Sciences (EUCASS), 2019
92019
Feasibility assessment of rapid Earth–Mars transfers using high-power electric propulsion
N Bérend, EC Moreno, JM Ruault, R Epenoy
Journal of Spacecraft and Rockets 51 (3), 946-957, 2014
92014
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