A 3-AXIS SATELLITE ATTITUDE CONTROL USING CATCS

被引：0

作者：

Bashaal-Khodari, Saleh ^{[1
]}

Varatharajoo, Renuganth ^{[1
]}

机构：

[1] Univ Putra Malaysia, Fac Engn, Dept Aerosp Engn, Upm Serdang 43400, Selangor, Malaysia

来源：

JBIS-JOURNAL OF THE BRITISH INTERPLANETARY SOCIETY | 2008年 / 61卷 / 11期

关键词：

Spacecraft; attitude control; thermal control; CATCS;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A 3-axis attitude control for a small satellite using combined attitude and thermal control system (CATCS) is presented in this paper. The CATCS system is designed to couple the attitude and the thermal control systems in one system. The CATCS principle is based on the use of the onboard excess heat to circulate a fluid inside a closed duct under the influence of generated current and magnetic flux fields. Till to date, the use of CATCS has been demonstrated for a single axis attitude control of a small satellite. The complete onboard 3-axis attitude control architecture based on the PI-controllers is implemented and numerically tested to enhance the closed-loop attitude control response of a satellite. The simulated attitude performances show that the CATCS system is able to perform the 3-axis attitude control of a satellite.

引用

页码：452 / 457

页数：6

共 13 条

[1]

CHRISTIAN JA, 2004, AIAA GUID NAV CONTR

[2] SPACECRAFT ATTITUDE-CONTROL AND STABILIZATION - APPLICATIONS OF GEOMETRIC CONTROL-THEORY TO RIGID BODY MODELS [J].

CROUCH, PE .

IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1984, 29 (04) :321-331

[3]

GONCHAROV K, 2004, 55 INT ASTR C VANC C

[4] Spacecraft attitude control using explicit model predictive control [J].

Hegrenæs, O ;

Gravdahl, JT ;

Tondel, P .

AUTOMATICA, 2005, 41 (12) :2107-2114

[5]

KULKARNI J, 2004, IEEE C DEC CONTR DEC

[6] Time-optimal magnetic attitude control for small spacecraft [J].

Liang, JS ;

Fullmer, R ;

Chen, YQ .

2004 43RD IEEE CONFERENCE ON DECISION AND CONTROL (CDC), VOLS 1-5, 2004, :255-260

[7] Microelectromechanical devices for satellite thermal control [J].

Osiander, R ;

Firebaugh, SL ;

Champion, JL ;

Farrar, D ;

Darrin, MAG .

IEEE SENSORS JOURNAL, 2004, 4 (04) :525-531

[8]

Sidi M. J., 1997, Spacecraft dynamics and control: a practical engineering approach, V7, DOI DOI 10.1017/CBO9780511815652

[9] Nonlinear adaptive spacecraft attitude control using solar radiation pressure [J].

Singh, SN ;

Yim, W .

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2005, 41 (03) :770-779

[10] Approach for combining spacecraft attitude and thermal control systems [J].

Varatharajoo, R ;

Kahle, R ;

Fasoulas, S .

JOURNAL OF SPACECRAFT AND ROCKETS, 2003, 40 (05) :657-664

← 1 2 →