FORMATION FLYING: RELATIVE ORBITS' MODELLING AND CONTROL THROUGH EULERIAN ORBITAL ELEMENTS

被引：0
|
作者：
Gaias, Gabriella V. M. [1 ]
Lavagna, Michele R. [1 ]
Golikov, Alexei R. [2 ]
Ovchinnikov, Michael Yu. [3 ]
机构：
[1] Politecn Milan, DIA Dipartimento Ingn Aerosp, Via La Masa 34, I-20156 Milan, Italy
[2] Russian Acad Sci, KIAM Ballist Ctr, Moscow 125047, Russia
[3] Russian Acad Sci, Keldysh Inst Appl Math, Sci Attitude Control Syst & Orientat Div, Moscow 125047, Russia
来源：
SPACEFLIGHT MECHANICS 2009, VOL 134, PTS I-III | 2009年 / 134卷
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D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
This work deals with the dynamics of spacecrafts in formation. The relative motion is described through the difference between the Eulerian orbital elements of the deputy satellite and the chief's ones. Eulerian orbital elements are defined from the constants of motion of the Intermediary Motion: they include perturbations till part of the 4th zonal harmonic of the Earth's gravity potential. A target relative motion insensitive up to the J(3) is defined by matching the time variations of the Eulerian angular elements. Reconfiguration manoeuvres are performed by a relative orbit control where errors in the orbital elements are feed-back.
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页码：1271 / +
页数：2
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