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Published in 2018 at "CEAS Space Journal"
DOI: 10.1007/s12567-017-0160-x
Abstract: The European Space Agency (ESA) is currently involved in several activities related to launch vehicle designs (Future Launcher Preparatory Program, Ariane 6, VEGA evolutions, etc.). Within these activities, ESA has identified the importance of developing…
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Keywords:
design gnc;
vehicle design;
analysis;
vehicle ... See more keywords
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1
Published in 2019 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2019.03.073
Abstract: Abstract The ability to perform safe landing is of great concern for reusable launch vehicles and landers; however, sloped terrains severely limit the degree of landing safety. To ensure that the launch vehicle and lander…
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Keywords:
landing gear;
landing;
launch vehicle;
adaptive landing ... See more keywords
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Published in 2020 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2020.07.022
Abstract: Abstract The Two-Stage-To-Orbit (TSTO) hypersonic vehicle is an example of a Reusable Launch Vehicle (RLVs) configuration, and it has the advantages of small mass and large payload. A TSTO concept aircraft comprising a booster and…
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Keywords:
nose configurations;
vehicle;
reusable launch;
launch vehicle ... See more keywords
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Published in 2020 at "Applied Acoustics"
DOI: 10.1016/j.apacoust.2020.107480
Abstract: Abstract The field of data compression has been evolved over the last decades. In this way, several techniques to reduce the amount of acquired data from the sensor required to be transmitted have been developed.…
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Keywords:
study launch;
vehicle board;
data compression;
launch vehicle ... See more keywords
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Published in 2021 at "Advances in Space Research"
DOI: 10.1016/j.asr.2020.10.006
Abstract: Abstract A Reusable Launch Vehicle (RLV), during the re-entry phase of its flight, experiences uncertain environment and extreme turbulence. This calls for an effective control strategy to guide the vehicle efficiently on a trajectory that…
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Keywords:
vehicle;
reusable launch;
entry trajectory;
launch vehicle ... See more keywords
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Published in 2017 at "IFAC-PapersOnLine"
DOI: 10.1016/j.ifacol.2017.08.095
Abstract: In this paper, we propose a strategy to solve endo-atmospheric launch vehicle optimal control problems using indirect methods. More specifically, we combine shooting methods with an adequate continuation algorithm, taking advantage of the knowledge of…
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Keywords:
atmospheric launch;
continuation;
endo atmospheric;
launch vehicle ... See more keywords
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Published in 2018 at "Journal of Aerospace Engineering"
DOI: 10.1061/(asce)as.1943-5525.0000825
Abstract: AbstractA dynamic model is proposed and validated to analyze the landing performance of a vertical landing reusable launch vehicle (RLV) with a novel oleo-honeycomb two-stage damper. Based on this ...
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Keywords:
vertical landing;
oleo honeycomb;
landing reusable;
reusable launch ... See more keywords
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Published in 2021 at "Aircraft Engineering and Aerospace Technology"
DOI: 10.1108/aeat-01-2021-0004
Abstract: The capability to predict and evaluate various configurations’ performance during the conceptual design phase using multidisciplinary design analysis and optimization can significantly increase the preliminary design process’s efficiency and reduce design and development costs. This…
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Keywords:
optimization;
launch vehicle;
multidisciplinary design;
design ... See more keywords
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Published in 2018 at "Aircraft Engineering and Aerospace Technology"
DOI: 10.1108/aeat-11-2016-0232
Abstract: Purpose This activity dealt with the thermal analysis of the launch vehicle (LV) Vega C through a lumped parameter model. The Vega C is the upgrade of the actual LV Vega within the Vega Consolidation…
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Keywords:
vega;
analysis launch;
analysis;
thermal analysis ... See more keywords
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Published in 2020 at "IEEE Transactions on Automatic Control"
DOI: 10.1109/tac.2019.2929099
Abstract: In this paper, we develop a geometric analysis and a numerical algorithm, based on indirect methods, to solve optimal guidance of endoatmospheric launch vehicle systems under mixed control-state constraints. Two main difficulties are addressed. First,…
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Keywords:
control;
optimal control;
launch vehicle;
endoatmospheric launch ... See more keywords
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Published in 2022 at "IEEE Transactions on Aerospace and Electronic Systems"
DOI: 10.1109/taes.2021.3126567
Abstract: This article focuses on the 3-D guidance strategy for a reusable launch vehicle (RLV) during terminal area energy management (TAEM) phase. Based on sliding-mode and shrinking-horizon techniques, the proposed scheme consists of trajectory generation and…
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Keywords:
launch vehicle;
reusable launch;
guidance;
domain ... See more keywords