Pseudospectral Convex Optimization for Powered Descent and Landing M Sagliano
Journal of Guidance, Control, and Dynamics 41 (2), 320-334, 2018
110 2018 Generalized M Sagliano
Journal of Guidance, Control, and Dynamics 42 (7), 1562-1570, 2019
75 2019 Adaptive disturbance-based high-order sliding-mode control for hypersonic-entry vehicles M Sagliano, E Mooij, S Theil
Journal of Guidance, Control, and Dynamics 40 (3), 521-536, 2017
59 2017 Optimal drag-energy entry guidance via pseudospectral convex optimization M Sagliano, E Mooij
Aerospace Science and Technology 117, 106946, 2021
55 2021 Onboard trajectory generation for entry vehicles via adaptive multivariate pseudospectral interpolation M Sagliano, E Mooij, S Theil
Journal of Guidance, Control, and Dynamics 40 (2), 466-476, 2016
47 2016 Onboard guidance for reusable rockets: aerodynamic descent and powered landing M Sagliano, A Heidecker, J Macés Hernández, S Farì, M Schlotterer, ...
AIAA Scitech 2021 Forum, 0862, 2021
36 2021 CALLISTO: a demonstrator for reusable launcher key technologies E Dumont, S Ishimoto, P Tatiossian, J Klevanski, B Reimann, T Ecker, ...
Transactions of the Japan Society for Aeronautical and Space Sciences …, 2021
32 2021 Survey of autonomous guidance methods for powered planetary landing Z Song, C Wang, S Theil, D Seelbinder, M Sagliano, X Liu, Z Shao
Frontiers of Information Technology & Electronic Engineering 21 (5), 652-674, 2020
29 2020 On the Radau pseudospectral method: theoretical and implementation advances M Sagliano, S Theil, M Bergsma, V D’Onofrio, L Whittle, G Viavattene
CEAS Space Journal 9, 313-331, 2017
28 2017 Safe landing area determination for a moon lander by reachability analysis YE Arslantaş, T Oehlschlägel, M Sagliano
Acta Astronautica 128, 607-615, 2016
23 2016 Hybrid jacobian computation for fast optimal trajectories generation M Sagliano, S Theil
AIAA Guidance, Navigation, and Control (GNC) Conference, 4554, 2013
22 2013 Spartan: A novel pseudospectral algorithm for entry, descent, and landing analysis M Sagliano, S Theil, V D’Onofrio, M Bergsma
Advances in Aerospace Guidance, Navigation and Control: Selected Papers of …, 2018
20 2018 DLR reusability flight experiment ReFEx W Bauer, P Rickmers, A Kallenbach, S Stappert, V Wartemann, ...
Acta Astronautica 168, 57-68, 2020
19 2020 Performance analysis of linear and nonlinear techniques for automatic scaling of discretized control problems M Sagliano
Operations Research Letters 42 (3), 213-216, 2014
17 2014 Spartan: an improved global pseudospectral algorithm for high-fidelity entry-descent-landing guidance analysis L Huneker, M Sagliano, Y Arslantas
16 2015 Simulations and flight tests of a new nonlinear controller for the EAGLE lander M Sagliano, M Dumke, S Theil
Journal of Spacecraft and Rockets 56 (1), 259-272, 2019
15 2019 Development of a novel algorithm for high performance reentry guidance M Sagliano
University of Bremen, 2016
15 2016 Guidance and control strategy for the CALLISTO flight experiment M Sagliano, T Tsukamoto, JA Maces Hernandez, D Seelbinder, ...
EUCASS Association, 2019
13 2019 Shefex-3 optimal feedback entry guidance M Sagliano, M Samaan, S Theil, E Mooij
AIAA space 2014 conference and exposition, 4208, 2014
12 2014 Robust control for reusable rockets via structured h-infinity synthesis M Sagliano, T Tsukamoto, A Heidecker, JA Maces Hernandez, S Fari, ...
11 2021 
Stephan TheilAbteilungsleiter Navigations- und Regelungssysteme, Institute für Raumfahrtsysteme, Deutsches Zentrum für Luft- und RaumfahrtVerified email at dlr.de
