Direct Indirect Hybrid Strategy for Optimal Powered Descent and Landing

Spada, Fabio and Sagliano, Marco and Topputo, Francesco (2023) Direct Indirect Hybrid Strategy for Optimal Powered Descent and Landing. Journal of Spacecraft and Rockets. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.A35650. ISSN 0022-4650.

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Official URL: https://arc.aiaa.org/doi/10.2514/1.A35650

Item URL in elib:

https://elib.dlr.de/197216/

Document Type:

Article

Title:

Direct Indirect Hybrid Strategy for Optimal Powered Descent and Landing

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Spada, Fabio	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Sagliano, Marco	UNSPECIFIED	https://orcid.org/0000-0003-1026-0693	UNSPECIFIED
Topputo, Francesco	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

July 2023

Journal or Publication Title:

Journal of Spacecraft and Rockets

Refereed publication:

Yes

Open Access:

Yes

Gold Open Access:

In SCOPUS:

Yes

In ISI Web of Science:

Yes

DOI:

10.2514/1.A35650

Publisher:

American Institute of Aeronautics and Astronautics (AIAA)

Series Name:

American Institute for Aeronautics and Astronautics

ISSN:

0022-4650

Status:

Published

Keywords:

Direct Indirect methods, Convex Optimization, Trajectory Optimization, Reusable Rockets, Powered Descent and Landing

HGF - Research field:

Aeronautics, Space and Transport

HGF - Program:

Space

HGF - Program Themes:

Space Transportation

DLR - Research area:

Raumfahrt

DLR - Program:

R RP - Space Transportation

DLR - Research theme (Project):

R - Project CALLISTO [RP]

Location:

Bremen

Institutes and Institutions:

Institute of Space Systems > Navigation and Control Systems

Deposited By:

Sagliano, Marco

Deposited On:

12 Sep 2023 12:03

Last Modified:

06 Oct 2023 12:32

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