In the article described the method of determination of fuel axpense of aircraft from the condition of motion of soluid in relation to the center of the masses considered. Using intellectual measuring elements based on magnetoelastic transformers builded in the construction of the controlled structural module as single whole, measure their state of loading and identify mass of object in a present moment of time, and by the known sizes of component aggregates of rocket, the location of resulting resultant rocket (center of the masses) determined in relation to the controlled axis of symmetry.

Proceedings of the Second World Congress "Aviation in the X X I-st Century" "Safety in Aviation", September 19-21, 2005 [Текст] = Матеріали Другого Всесвітнього конгресу "Авіація ХХІ століття" "Безпека в авіації" / International Civil Aviation Organization; Ministry of Education and Science of Ukraine; National Academy of Sciences of Ukraine; National Aviation University. — Kyiv : NAU, 2005. — 481 p. : il.