Trajectory assessment and optimisation in the context of small launcher design

Trajectory assessment and optimisation in the context of small launcher design

The paper presents a mathematical model that can be used to quickly define a nominal trajectory for the studied small launcher configuration. The tool developed based on the proposed mathematical model can be used separately for trajectory assessments or it can be integrated in a multidisciplinary o...

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Veröffentlicht in:INCAS bulletin 2020-06, Vol.12 (2), p.117-132
Hauptverfasser: ONEL, Alexandru-Iulian, CHELARU, Teodor-Viorel
Format: Artikel
Sprache:eng
Schlagworte:
Algorithms
Design optimization
Launchers
Mathematical analysis
mathematical model
Mathematical models
multidisciplinary optimisation
orbital performance
Satellites
small launcher
Trajectory analysis
trajectory assessment
Trajectory optimization
Velocity
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Beschreibung
Zusammenfassung:The paper presents a mathematical model that can be used to quickly define a nominal trajectory for the studied small launcher configuration. The tool developed based on the proposed mathematical model can be used separately for trajectory assessments or it can be integrated in a multidisciplinary optimisation algorithm for a preliminary small launcher design, together with the trajectory optimisation for a maximum orbital performance.
ISSN:2066-8201
2247-4528
DOI:10.13111/2066-8201.2020.12.2.10