Zobrazeno 1 - 10
of 34
pro vyhledávání: '"Marco Sagliano"'
Autor:
Marco Sagliano
Publikováno v:
Aerospace, Vol 11, Iss 10, p 863 (2024)
The interdisciplinary field known as Guidance, Navigation, and Control (GNC) has been one of the key contributors to the tremendous advancements in space exploration since the inception of the Mercury and Apollo programs [...]
Externí odkaz:
https://doaj.org/article/f830fdab7f604601a4e8bb61a1f8e563
Autor:
Stefano Farì, Marco Sagliano, José Alfredo Macés Hernández, Anton Schneider, Ansgar Heidecker, Markus Schlotterer, Svenja Woicke
Publikováno v:
Aerospace, Vol 11, Iss 5, p 337 (2024)
Reusable rockets must rely on well-designed Guidance, Navigation and Control (GNC) algorithms. Because they are tested and verified in closed-loop, high-fidelity simulators, emphasizing the strategy to achieve such advanced models is of paramount imp
Externí odkaz:
https://doaj.org/article/648183a2711946e5bcb81384564e8e5e
Publikováno v:
Modelling and Simulation in Engineering, Vol 2020 (2020)
This paper proposes an algorithm for modeling a three-dimensional tethered environment for testing vertical-take off, vertical landing vehicles. The method is able to take several geometrical configurations into account and combines the classical cat
Externí odkaz:
https://doaj.org/article/5be8616658d24370ba7b4c939ce61d68
Autor:
Marco Sagliano, José A. Macés Hernández, Stefano Farì, Ansgar Heidecker, Markus Schlotterer, Svenja Woicke, David Seelbinder, Sven Krummen, Etienne Dumont
Publikováno v:
Journal of Guidance, Control, and Dynamics. 46:815-837
This paper investigates the use of structured robust techniques for the control design of the aerodynamic descent phase of a reusable rocket. A unified control strategy based on the use of linear-time-invariant structured [Formula: see text] controll
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1a6d6873a45339c5bda7b18eea39aa84
https://doi.org/10.2514/1.g007077
https://doi.org/10.2514/1.g007077
Publikováno v:
AIAA SCITECH 2023 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0de1b772e34f972cd807bb7f17ab47ea
https://doi.org/10.2514/6.2023-2502
https://doi.org/10.2514/6.2023-2502
Publikováno v:
AIAA SCITECH 2023 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f664d950873e8f975e0cdb8698c9fd41
https://doi.org/10.2514/6.2023-2005
https://doi.org/10.2514/6.2023-2005
Publikováno v:
Autonomous Trajectory Planning and Guidance Control for Launch Vehicles ISBN: 9789819906123
This chapter expands our development of an autonomous descent guidance algorithm which is able to deal with both the aerodynamic descent and the powered landing phases of a reusable rocket. The method uses sequential convex optimization applied to a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::32306d1374c9d7ba38b01e3d318d4176
https://doi.org/10.1007/978-981-99-0613-0_5
https://doi.org/10.1007/978-981-99-0613-0_5
Autor:
Marco Sagliano, Piyapat Saranrittichai, Michael Dumke, Stephan Theil, Guilherme Fragoso Trigo
Publikováno v:
CEAS Space Journal. 12:97-113
Precise landing on planets, moons, and other larger celestial bodies requires powered descent, hovering, and vertical landing. Similarly, recent and future concepts for re-usable launch vehicle (RLVs) also involve a vertical take-off and landing. The
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5380f55d033e84bcfdf2e7c85eb6acc6
https://doi.org/10.1007/s12567-019-00269-5
https://doi.org/10.1007/s12567-019-00269-5
Autor:
Marco Sagliano
Publikováno v:
Scopus-Elsevier
This paper wants to be a tribute to the Apollo 11 mission, that celebrated its 50th anniversary in 2019. By using modern methods based on numerical optimization we reconstruct critical phases of the original mission, and more specifically the ascent
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::971172abdf85ac65d14bb65cdc87b262
https://elib.dlr.de/140508/
https://elib.dlr.de/140508/
Autor:
Marco Sagliano, José V. Garrido
This paper illustrates the trajectory modeling of multistage rockets for both ascent anddescent phases. The computation of solutions is performed by coupling a multiphase optimal-control problem formulation with a transcription performed via Radau ps
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0d3c01efe48a90b4bef0f51d8a20a20a
https://elib.dlr.de/140558/
https://elib.dlr.de/140558/