Generalized Attitude Model for Momentum-Biased Solar Sail Spacecraft

被引：26

作者：

Ono, Go ^{[1
]}

Tsuda, Yuichi ^{[2
]}

Akatsuka, Kosuke ^{[3
]}

Saiki, Takanao ^{[2
]}

Mimasu, Yuya ^{[2
]}

Ogawa, Naoko ^{[2
]}

Terui, Fuyuto ^{[2
]}

机构：

[1] Japan Aerosp Explorat Agcy, 2-1-1 Sengen, Tsukuba, Ibaraki 3058505, Japan

[2] Japan Aerosp Explorat Agcy, Chuo Ku, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 2525210, Japan

[3] Univ Tokyo, Bunkyo Ku, 7-3-1 Hongo, Tokyo 1138654, Japan

来源：

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

基金：

日本学术振兴会;

关键词：

DYNAMICS; SYSTEM;

D O I：

10.2514/1.G001750

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper describes a method of modeling general attitude dynamics of a nonspinning momentum-biased spacecraft under strong influence of solar radiation pressure. This model, called the "generalized sail dynamics model," can be applied to realistic solar sail spacecraft with nonflat surfaces and nonuniform optical reflectance. A coarse sun-pointing momentum-biased spacecraft is especially of interest, for which an approximate solution of the equations of motion is analytically derived. Stability and fundamental characteristics of momentum-biased spacecraft dynamics as well as theoretical relations with past dynamics models are discussed in detail. Furthermore, unique attitude motion predicted by the novel model is verified with flight data of the Japanese interplanetary probe, Hayabusa 2.

引用

页码：1491 / 1500

页数：10

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