SINGLE-IMPULSE TRANSFER TO A NOMINALLY PERIODIC ORBIT NEAR THE POINT L2 IN THE SUN-EARTH SYSTEM AND ASSOCIATED PROBLEMS.

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作者
Lidov, M.L.
Lyakhova, V.A.
Teslenko, N.M.
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MATHEMATICAL TECHNIQUES - Estimation;
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Problems related to transferring to and maintaining the orbit of a spacecraft near the collinear libration point L//2 of the earth-sun system are considered. A method is developed for analyzing and calculating single-impulse transfer of a spacecraft from an intermediate orbit to a nominally periodic orbit that is closest to L//2. A method is obtained for calculating the motion of a spacecraft along a nominally periodic orbit for a sufficiently long duration of time. Estimates are obtained for the characteristics of monoparametric correction of the transfer trajectory that compensates for errors in making the transfer.
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页码:129 / 148
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