Experimental study on line-of-sight (LOS) attitude control using control moment gyros under micro-gravity environment

被引：12
作者：
Kojima, Hirohisa [1 ]
Hiraiwa, Kana [1 ]
Yoshimura, Yasuhiro [1 ]
机构：
[1] Tokyo Metropolitan Univ, Dept Aerosp Engn, 6-6 Asahigaoka, Hino, Tokyo 1910065, Japan
来源：
ACTA ASTRONAUTICA | 2018年 / 143卷
关键词：
W-Z parameters; Control moment gyro; Line of sight; Attitude maneuver; Micro-gravity experiment; 2 CONTROL TORQUES; RIGID SPACECRAFT; ANGULAR VELOCITY; FEEDBACK STABILIZATION; BODY;
D O I：
10.1016/j.actaastro.2017.11.020
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
This paper presents the results of line-of-sight (LOS) attitude control using control moment gyros under a micro gravity environment generated by parabolic flight. The W-Z parameters are used to describe the spacecraft attitude. In order to stabilize the current LOS to the target LOS, backstepping-based feedback control is considered using the W-Z parameters. Numerical simulations and experiments under a micro-gravity environment are carried out, and their results are compared in order to validate the proposed control methods.
引用
收藏
页码：118 / 125
页数：8
相关论文
共 31 条
[1]   COMMENTS ON THE STABILIZABILITY OF THE ANGULAR VELOCITY OF A RIGID BODY [J].
AEYELS, D ;
SZAFRANSKI, M .
SYSTEMS & CONTROL LETTERS, 1988, 10 (01) :35-39
[2]   STABILIZATION BY SMOOTH FEEDBACK OF THE ANGULAR VELOCITY OF A RIGID BODY [J].
AEYELS, D .
SYSTEMS & CONTROL LETTERS, 1985, 6 (01) :59-63
[3]   Robust stabilization of the angular velocity of a rigid body [J].
Astolfi, A ;
Rapaport, A .
SYSTEMS & CONTROL LETTERS, 1998, 34 (05) :257-264
[4]   Output feedback stabilization of the angular velocity of a rigid body [J].
Astolfi, A .
SYSTEMS & CONTROL LETTERS, 1999, 36 (03) :181-192
[5]   ON THE ATTITUDE STABILIZATION OF RIGID SPACECRAFT [J].
BYRNES, CI ;
ISIDORI, A .
AUTOMATICA, 1991, 27 (01) :87-95
[6]   Explicit feedbacks stabilizing the attitude of a rigid spacecraft with two control torques [J].
Coron, JM ;
Kerai, EY .
AUTOMATICA, 1996, 32 (05) :669-677
[7]   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
[8]  
Gui H., 2013, 20134794 AIAA
[9]   Attitude Stabilization of a Spacecraft with Two Parallel Control Moment Gyroscopes [J].
Gui, Haichao ;
Vukovich, George ;
Xu, Shijie .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2016, 39 (03) :724-731
[10]   On the attitude stabilization of a rigid spacecraft using two skew control moment gyros [J].
Gui, Haichao ;
Jin, Lei ;
Xu, Shijie ;
Zhang, Jun .
NONLINEAR DYNAMICS, 2015, 79 (03) :2079-2097
1234