Multiple-Spacecraft Orbit-Transfer Problem: The No-Booster Case

1999 ◽  
Vol 22 (5) ◽  
pp. 650-657 ◽  
Author(s):  
Cesar A. Ocampo ◽  
George W. Rosborough
2016 ◽  
Vol 39 (8) ◽  
pp. 1734-1743 ◽  
Author(s):  
M. Avendaño ◽  
V. Martín-Molina ◽  
J. Martín-Morales ◽  
J. Ortigas-Galindo

1994 ◽  
Vol 17 (5) ◽  
pp. 1075-1081 ◽  
Author(s):  
Antonio F. B. A. Prado ◽  
Roger A. Broucke

2012 ◽  
Vol 2012 ◽  
pp. 1-9 ◽  
Author(s):  
Weijun Huang

The coplanar orbit transfer problem has been an important topic in astrodynamics since the beginning of the space era. Though many approximate solutions for power-limited orbit transfer problem have been developed, most of them rely on simplifications of the dynamics of the problem. This paper proposes a new approximation method called primer vector approximation method to solve the classic power-limited orbit transfer problem. This method makes no simplification on the dynamics, but instead approximates the optimal primer-vector function. With this method, this paper derives two approximate solutions for the power-limited orbit transfer problem. Numerical tests show the robustness and accuracy of the approximations.


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