Maximum Likelihood-Based Worst-Case Optimization Design of Hydrazine Propulsion System for aSatellite Orbital Transfer System under Uncertainty

In this paper, a design of a hydrazine monopropellant system is proposed based on the maximum likelihood for the presentation of uncertainties, without any specific assumptions about the type of distribution and even uncertainty in distribution parameters by the johnson distributions family. The max...

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Bibliografische Detailangaben

Hauptverfasser:	Alireza Toloei, Mohammad Fatehi, Behrooz Keshtegar
Format:	Artigo
Sprache:	Persa
Veröffentlicht:	Aerospace Research Institute 2021-09-01
Schriftenreihe:	فصلنامه علوم و فناوری فضایی
Schlagworte:	"worst-case optimization" " mono propellant propulsion system" " maximum likelihood" "uncertainty"
Online-Zugang:	https://jsst.ias.ir/article_122459_af97266b7d9bf478920d5a3b42aff418.pdf
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