Space systems design (spacecraft, satellites, space stations and their equipment)
Maximum Likelihood-Based Worst-Case Optimization Design of Hydrazine Propulsion System for aSatellite Orbital Transfer System under Uncertainty

Alireza Toloei; Mohammad Fatehi; Behrooz Keshtegar

Volume 14, Issue 3 , September 2021, , Pages 1-14

Abstract
  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 maximum ...  Read More