Optimal Multiple-Impulse Circular Orbit Phasing

被引：2

作者：

Trofimov, Sergey P. ^{[1
]}

Ovchinnikov, Mikhail Yu. ^{[2
]}

机构：

[1] Keldysh Inst Appl Math, Spaceflight Mech & Control Dept, 4 Miusskaya Pl, Moscow 125047, Russia

[2] Keldysh Inst Appl Math, Spaceflight Mech & Control Dept, Attitude Control Syst & Orientat Div, 4 Miusskaya Pl, Moscow 125047, Russia

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2016年 / 39卷 / 07期

基金：

俄罗斯科学基金会;

关键词：

OPTIMAL; 2-IMPULSE; VICINITY;

D O I：

10.2514/1.G001513

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A study considers the fundamental problem of circular orbit phasing by performing a multiple-impulse maneuver. It is shown below that the peculiar properties of the considered problem allow a simpler procedure of finding the globally optimal solution. It appears to be composed of two- and four-impulse maneuvers and switches between them as the phasing maneuver duration grows. Two-impulse maneuvers do not require any optimization, as they are unambiguously calculated as least-delta-v solutions to the multiple-revolution Lambert problem.

引用

页码：1675 / +

页数：4

共 14 条

[1]

Baranov A., 1995, COSMIC RES+, P382

[2] Quadratic-based computation of four-impulse optimal rendezvous near circular orbit [J].