Optimum low-thrust transfers between neighboring coplanar circular orbits were studied for simplified system model; within limits of assumptions made, numerical results are sufficient to describe optimum thrust steering program and performance capability of vehicle in terms of its thrust/weight ratio, orbital frequency, and thrust duration.
Optimal low-thrust near-circular orbital transfer
AIAA J
AIAA Journal ; 1 , n 6
1963
5 pages
Article (Journal)
English
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