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Publication

Tech. report, 2006
Publisher:
Тезисы доклада на 11 международной конференции 'Системный анализ, навигация,управление'. (Евпатория 2006)
Authors: Akhmetshin R. Z.
The use of ideal low thrust model for definition of optimal stepped program of low thrust
Abstract:
The ideal low thrust model affords some facilities for investigation of optimal flights of spacecraft with stepped low thrust. It allows to get a majorant estimate of the functional – the final spacecraft mass, and to understand how well is the choice of electro-rocket parameters.
Publication language: russian
Research direction:
Theoretical and applied problems of mechanics
Source text:
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