I agree that this site is using cookies. You can find further informations
here
.
X
Login
My folder (
0
)
Home
About us
Home About us
Our history
Profile
Press & public relations
Friends
The library in figures
Exhibitions
Projects
Training, internships, careers
Films
Services & Information
Home Services & Information
Lending and interlibrary loans
Returns and renewals
Training and library tours
My Account
Library cards
New to the library?
Download Information
Opening hours
Learning spaces
PC, WLAN, copy, scan and print
Catalogs and collections
Home Catalogs and Collections
Rare books and manuscripts
Digital collections
Subject Areas
Our sites
Home Our sites
Central Library
Law Library (Juridicum)
BB Business and Economics (BB11)
BB Physics and Electrical Engineering
TB Engineering and Social Sciences
TB Economics and Nautical Sciences
TB Music
TB Art & Design
TB Bremerhaven
Contact the library
Home Contact the library
Staff Directory
Open access & publishing
Home Open access & publishing
Reference management: Citavi & RefWorks
Publishing documents
Open Access in Bremen
Show Desktop-Version
Toggle navigation
Celani, Fabio
123
results:
Search for persons
X
Format
Online (123)
Mediatypes
Articles (Online) (24)
OpenAccess-fulltext (99)
Sorted by: Relevance
Sorted by: Year
?
1
Lunar descent and landing via two-phase explicit guidance a..:
Pontani, Mauro
;
Celani, Fabio
;
Carletta, Stefano
Acta Astronautica. 212 (2023) - p. 672-685 , 2023
Link:
https://doi.org/10.1016/..
?
2
Quaternion versus Rotation Matrix Feedback for Spacecraft A..:
Celani, Fabio
Aerospace. 9 (2022) 1 - p. 24 , 2022
Link:
https://doi.org/10.3390/..
?
3
Minimum-Time Spacecraft Attitude Motion Planning Using Obje..:
Celani, Fabio
;
Bruni, Renato
Journal of Optimization Theory and Applications. 191 (2021) 2-3 - p. 776-793 , 2021
Link:
https://doi.org/10.1007/..
?
4
Neighboring Optimal Guidance and Constrained Attitude Contr..:
Pontani, Mauro
;
Celani, Fabio
Aerotecnica Missili & Spazio. 100 (2021) 2 - p. 131-146 , 2021
Link:
https://doi.org/10.1007/..
?
5
Variable-time-domain neighboring optimal guidance and attit..:
Pontani, Mauro
;
Celani, Fabio
Acta Astronautica. 175 (2020) - p. 616-626 , 2020
Link:
https://doi.org/10.1016/..
?
6
Gain Selection for Attitude Stabilization of Earth-Pointing..:
Celani, Fabio
Aerotecnica Missili & Spazio. 100 (2020) 1 - p. 15-24 , 2020
Link:
https://doi.org/10.1007/..
?
7
Spacecraft Attitude Motion Planning Using Gradient-Based Op..:
Celani, Fabio
;
Lucarelli, Dennis
Journal of Guidance, Control, and Dynamics. 43 (2020) 1 - p. 140-145 , 2020
Link:
https://doi.org/10.2514/..
?
8
Combining Global and Local Strategies to Optimize Parameter..:
Bruni, Renato
;
Celani, Fabio
Journal of Optimization Theory and Applications. 181 (2019) 3 - p. 997-1014 , 2019
Link:
https://doi.org/10.1007/..
?
9
Neighboring optimal guidance and constrained attitude contr..:
Pontani, Mauro
;
Celani, Fabio
Acta Astronautica. 156 (2019) - p. 78-91 , 2019
Link:
https://doi.org/10.1016/..
?
10
Global and robust attitude control of a launch vehicle in e..:
Celani, Fabio
Aerospace Science and Technology. 74 (2018) - p. 22-36 , 2018
Link:
https://doi.org/10.1016/..
?
11
Spacecraft Attitude Stabilization with Piecewise-Constant M..:
Celani, Fabio
Journal of Guidance, Control, and Dynamics. 39 (2016) 5 - p. 1140-1146 , 2016
Link:
https://doi.org/10.2514/..
?
12
A Robust Optimization Approach for Magnetic Spacecraft Atti..:
Bruni, Renato
;
Celani, Fabio
Journal of Optimization Theory and Applications. 173 (2016) 3 - p. 994-1012 , 2016
Link:
https://doi.org/10.1007/..
?
13
Spacecraft Attitude Stabilization Using Magnetorquers with ..:
Celani, Fabio
Journal of Guidance, Control, and Dynamics. 39 (2016) 9 - p. 2184-2191 , 2016
Link:
https://doi.org/10.2514/..
?
14
Robust three-axis attitude stabilization for inertial point..:
Celani, Fabio
Acta Astronautica. 107 (2015) - p. 87-96 , 2015
Link:
https://doi.org/10.1016/..
?
15
Output regulation for the TORA benchmark via rotational pos..:
Celani, Fabio
Automatica. 47 (2011) 3 - p. 584-590 , 2011
Link:
https://doi.org/10.1016/..
1-15