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Tech. report, 2006
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
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
Russian source text: