ON THE SEMIPASSIVE ATTITUDE-CONTROL AND PROPULSION OF SPACE-VEHICLES USING SOLAR-RADIATION PRESSURE

被引：13

作者：

MODI, VJ

机构：

[1] Department of Mechanical Engineering, The University of British Columbia, Vancouver

来源：

ACTA ASTRONAUTICA | 1995年 / 35卷 / 2-3期

关键词：

D O I：

10.1016/0094-5765(94)00271-M

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper briefly reviews attitude dynamics and trajectory mechanics of spacecraft in the presence of environmental forces with particular emphasis on the solar radiation induced pressure and thermal effects on attitude dynamics. In general, the effect is destabilizing as indicated by a significant reduction in the size of the limiting integral manifold. However, several semi-passive controllers have been proposed which can use the environmental forces to advantage in stabilizing the system. Furthermore, the solar radiation-induced forces can be used to advantage for propulsion and trajectory transfer. Examples of contemporary interest illustrate effectiveness of the concepts in achieving desired attitude and trajectory.

引用

收藏

页码：231 / 246

页数：16

相关论文

共 50 条

[41] ATTITUDE CONTROL OF A SUN-POINTING SPINNING SPACECRAFT BY MEANS OF SOLAR RADIATION PRESSURE [J].

CROCKER, MC .

JOURNAL OF SPACECRAFT AND ROCKETS, 1970, 7 (03) :357-&

[42] MEASUREMENT OF THE GALACTIC COSMIC-RADIATION DOSE-RATE DURING THE 21ST SOLAR-ACTIVITY CYCLE ON PROGNOS SPACE-VEHICLES [J].

ANDRONOV, EA ;

BENGIN, VV ;

MURATOVA, IA ;

PETROV, VM ;

RYZHOVA, LI ;

SHUMSHUROV, VI .

KOSMICHESKAYA BIOLOGIYA I AVIAKOSMICHESKAYA MEDITSINA, 1988, 22 (05) :92-93

[43] DEVELOPMENT EXPERIENCE OF THE ATTITUDE-CONTROL SYSTEM USING SINGLE-AXIS CONTROL MOMENT GYROS FOR LONG-TERM ORBITING SPACE STATIONS [J].

BRANETS, VN ;

WEINBERG, DM ;

VERESTCHAGIN, VP ;

DANILOVNITUSOV, NN ;

LEGOSTAYEV, VP ;

PLATONOV, VN ;

SEMYONOV, YP ;

SEMYACHKIN, VS ;

CHERTOCK, BE ;

SHEREMETYEVSKY, NN .

ACTA ASTRONAUTICA, 1988, 18 :91-98

[44] Lunar Formation Control Using the Differential Solar Radiation Pressure [J].

Gurfil, Pini ;

Nie, Tao .

2019 27TH MEDITERRANEAN CONFERENCE ON CONTROL AND AUTOMATION (MED), 2019, :221-226

[45] STABILITY ANALYSIS AND SUN-TRACKING ATTITUDE CONTROL OF SPACECRAFT UNDER SOLAR RADIATION PRESSURE [J].

Hayashi, Naohiro ;

Ono, Go ;

Mimasu, Yuya ;

Kawaguchi, Jun'ichiro .

ASTRODYNAMICS 2013, PTS I-III, 2014, 150 :2045-2055

[46] REMOTE-SENSING OF CLOUD-TOP PRESSURE USING REFLECTED SOLAR-RADIATION IN THE OXYGEN A-BAND [J].

WU, MLC .

JOURNAL OF CLIMATE AND APPLIED METEOROLOGY, 1985, 24 (06) :539-546

[47] Shape control of slack space reflectors using modulated solar pressure [J].

Borggraefe, Andreas ;

Heiligers, Jeannette ;

Ceriotti, Matteo ;

McInnes, Colin R. .

PROCEEDINGS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES, 2015, 471 (2179)

[48] Using solar radiation pressure to control L2 orbits [J].

Tene, N ;

Richon, K ;

Folta, D ;

Tene, K .

SPACEFLIGHT DYNAMICS 1998, VOL 100, PART 1 AND 2, 1998, 100 :617-627

[49] Analysis of influence of solar radiation pressure on ground track keeping control in zero yaw attitude mode [J].

Zeng Guang ;

Wu Xinlin ;

Gong Bing ;

Li Donglin ;

Wang Chao .

CHINESE SPACE SCIENCE AND TECHNOLOGY, 2019, 39 (03) :23-29

[50] On-orbit verification of fuel-free attitude control system for spinning solar sail utilizing solar radiation pressure [J].

Funase, Ryu ;

Shirasawa, Yoji ;

Mimasu, Yuya ;

Mori, Osamu ;

Tsuda, Yuichi ;

Saiki, Takanao ;

Kawaguchi, Jun'ichiro .

ADVANCES IN SPACE RESEARCH, 2011, 48 (11) :1740-1746

← 1 2 3 4 5 →