To predict accurately free-flight motion of rocket near earth (or other oblate body) for trajectory design and guidance, gravitational effect of equatorial bulge must be accounted for; this can be done by solving equations of motion, based on gravitational potential model developed by J. P.Vinti; analysis is modified considerably to obtain solution suited to free-flight segments of ascent to satellite orbit, satellite de-orbit, ballistic missile, and spacecraft skip re-entry trajectories.
Vinti solution for free-flight rocket trajectories
AIAA J
AIAA Journal ; 1 , n 6
1963
4 pages
Article (Journal)
English
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VINTI SOLUTION FOR FREE-FLIGHT ROCKET TRAJECTORIES
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