OPTIMAL OPEN LOW-COST TWO-IMPULSE TRANSFERS IN A PLANE

被引:0
作者
Carter, Thomas E. [1 ]
Humi, Mayer [2 ]
机构
[1] Eastern Connecticut State Univ, Dept Math, Willimantic, CT 06226 USA
[2] Worcester Polytech Inst, Dept Math Sci, Worcester, MA 01609 USA
来源
ASTRODYNAMICS 2013, PTS I-III | 2014年 / 150卷
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The problem of finding a planar open optimal two-impulse transfer orbit between two known Keplerian orbits is found in terms of a set of necessary conditions for minimizing the total characteristic velocity of the transfer arcs and a test to pick the minimizing orbit from the extremals. The problem is open in the sense that the difference between the final and initial true anomaly is unbounded. Using a transformation of the variables presented in previous work, necessary conditions for an optimal transfer are determined, followed by a proof that an optimal transfer exists, concluding with some sufficiency arguments. Application of the work to non-circular elliptical boundary orbits reveals a set of boundary conditions that result in "low-cost" optimal transfers having velocity increments that are tangent to the boundary orbits at their apogees. These boundary conditions consist of only three types. A simple closed-form solution is provided for each type. More general boundary conditions that result in more complicated optimal solutions are to be discussed in a work that follows.
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收藏
页码:749 / 760
页数:12
相关论文
共 3 条
[1]  
Carter T., 2012, J CELESTIAL MECH DYN, V112, P385, DOI DOI 10.1007/S10569-012-9399-X
[2]  
Carter T., 2013, AAS AIAA ASTR SPEC C
[3]  
Humi M., OPTIMAL OPEN 2 UNPUB