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 |
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ASJC Scopus subject areas
- Engineering(all)
Cite this
OPTIMAL SPATIAL TURNING OF A SPACE VEHICLE RELATIVE TO CENTER OF MASS. / Shklyar, V. N.; Malyshenko, A. M.
Cosmic Res. Vol. 13 4. ed. 1975. p. 425-431.Research output: Chapter in Book/Report/Conference proceeding › Chapter
}
TY - CHAP
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.
UR - http://www.scopus.com/inward/record.url?scp=0016525721&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=0016525721&partnerID=8YFLogxK
M3 - Chapter
VL - 13
SP - 425
EP - 431
BT - Cosmic Res
ER -