Kharytonov O. Mathematical modeling and optimization of perspective high-thrust rocket engines of space vehicles

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0400U002892

Thesis Registration Form

0400U002892.pdf

Applicant for

Specialization

  • 01.05.04 - Системний аналіз і теорія оптимальних рішень

02-11-2000

Specialized Academic Board

Д 26.205.01

Essay

New mathematical models of nuclear and liquid rocket engines have been developed. With the help of these models the investigation of optimal control properties that are invariant to problem functional and boundary conditions has been carried out. To analyze the effeciency of optimal control a number of space flight mechanics model problems has been investigated.

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