On basis of first order analysis of equations of motion of restricted 3-body problem, solution is obtained for position and velocity components of motion as function of initial conditions; analytical results are compared with results obtained by numerical integration; suggestions given for scientific experiments performed with use of artificial satellites established in orbit about stable libration points.
Considerations of motion of small body in vicinity of stable libration points of earth-moon system
NASA -- Tech Report
1963
37 pages
Report
English
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Solar influence on satellite motion near stable earth-moon libration points
Engineering Index Backfile | 1964
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