Autonomous regulation of spacecraft motion about unstable periodic orbits using impulsive maneuvers

被引:0
作者
Fukuzawa, Hiroaki [1 ]
机构
[1] Estech Corp, Naka Ku, Yokohama, Kanagawa 2310023, Japan
来源
SPACEFLIGHT MECHANICS 2006, VOL 124, PTS 1 AND 2 | 2006年 / 124卷
关键词
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 paper presents a control method for autonomous regulation of spacecraft motion about unstable periodic orbits by occasional impulsive maneuvers. In this method, the impulsive maneuver to be applied at each prescribed time is obtained by modulating the difference between the actual state and the reference state of the motion at the time. The method is based on that of Generalized Sampled-data Hold Function (GSHF) control which is known to be useful in stabilizing motion about unstable periodic orbits using continuous maneuvers. A formula for impulsive maneuvers is obtained so that the impulsive maneuvers mimic the efficacy of a stabilizing GSHF controller. The method is applied to a halo orbit spacecraft in the Hill's circular three-body problem as an illustration.
引用
收藏
页码:1045 / 1060
页数:16
相关论文
共 21 条
[11]   CONTROL OF LINEAR-SYSTEMS USING GENERALIZED SAMPLED-DATA HOLD FUNCTIONS [J].
KABAMBA, PT .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1987, 32 (09) :772-783
[12]   MONODROMY EIGENVALUE ASSIGNMENT IN LINEAR PERIODIC-SYSTEMS [J].
KABAMBA, PT .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1986, 31 (10) :950-952
[13]  
Kulkarni J, 2004, P AMER CONTR CONF, P1025
[14]  
Lo MW, 2001, J ASTRONAUT SCI, V49, P169
[15]  
LO MW, 2005, AAS AIAA ASTR SPEC C
[16]  
Marchal C., 1990, The Three-Body Problem
[17]   Stabilizing motion relative to an unstable orbit: Applications to spacecraft formation flight [J].
Scheeres, DJ ;
Hsiao, FY ;
Vinh, NX .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2003, 26 (01) :62-73
[18]   Stability analysis of planetary satellite orbiters: Application to the Europa orbiter [J].
Scheeres, DJ ;
Guman, MD ;
Villac, BF .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2001, 24 (04) :778-787
[19]   The restricted Hill four-body problem with applications to the Earth-Moon-Sun system [J].
Scheeres, DJ .
CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 1998, 70 (02) :75-98
[20]  
SWIESEL W, 1983, J ASTRONAUT SCI, V31, P63