OPTIMAL SPATIAL TURNING OF A SPACE VEHICLE RELATIVE TO CENTER OF MASS.

Division for Automation and Robotics

Research output: Chapter in Book/Report/Conference proceeding › Chapter

Abstract

The spatial-turning problem for a space vehicle in the class of motions with two time-optimal successive turns is considered. Formulas are obtained to determine the parameters of successive turns and to estimate the rate of response and flow rate of the propulsive mass.

Original language	English
Title of host publication	Cosmic Res
Pages	425-431
Number of pages	7
Volume	13
Edition	4
Publication status	Published - Jul 1975

ASJC Scopus subject areas

Engineering(all)

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title = "OPTIMAL SPATIAL TURNING OF A SPACE VEHICLE RELATIVE TO CENTER OF MASS.",

abstract = "The spatial-turning problem for a space vehicle in the class of motions with two time-optimal successive turns is considered. Formulas are obtained to determine the parameters of successive turns and to estimate the rate of response and flow rate of the propulsive mass.",

author = "Shklyar, {V. N.} and Malyshenko, {A. M.}",

year = "1975",

month = jul,

language = "English",

volume = "13",

pages = "425--431",

booktitle = "Cosmic Res",

edition = "4",

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T1 - OPTIMAL SPATIAL TURNING OF A SPACE VEHICLE RELATIVE TO CENTER OF MASS.

AU - Shklyar, V. N.

AU - Malyshenko, A. M.

PY - 1975/7

Y1 - 1975/7

N2 - The spatial-turning problem for a space vehicle in the class of motions with two time-optimal successive turns is considered. Formulas are obtained to determine the parameters of successive turns and to estimate the rate of response and flow rate of the propulsive mass.

AB - The spatial-turning problem for a space vehicle in the class of motions with two time-optimal successive turns is considered. Formulas are obtained to determine the parameters of successive turns and to estimate the rate of response and flow rate of the propulsive mass.

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VL - 13

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EP - 431

BT - Cosmic Res

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