Abstract
The parameter dependency of large space structures on the coupling among attitude motion, structural vibration, and orbital motion has been investigated, particularly for structures such as tethered satellite systems. Tethered satellites are noticed for their possible applications. From space solar power systems to deorbit system, the applications of tethered satellites spread out over various fields. In this paper, we investigate planar motion of a satellite model, which consists of two tip particles and a massless spring. For such a space structure, the characteristics of the planar motion are shown to be determined by the mass ratio of tip particles, the natural frequency ratio of axial vibration to orbital motion, and the axial length ratio of the spring to the orbital radius. Among these three parameters, the natural frequency ratio has the greatest influence on the coupling phenomenon. Furthermore, the parameter range over which the coupling phenomenon occurs is specified.
| Original language | English |
|---|---|
| Pages (from-to) | 61-71 |
| Number of pages | 11 |
| Journal | Journal of Aerospace Engineering |
| Volume | 21 |
| Issue number | 2 |
| DOIs | |
| Publication status | Published - 2008 Mar 24 |
| Externally published | Yes |
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Keywords
- Aerospace engineering
- Space structures
- Structural dynamics
- Vibration
ASJC Scopus subject areas
- Civil and Structural Engineering
- Materials Science(all)
- Aerospace Engineering
- Mechanical Engineering
Cite this
Coupling among pitch motion, axial vibration, and orbital motion of large space structures. / Ishimura, Kosei; Higuchi, Ken.
In: Journal of Aerospace Engineering, Vol. 21, No. 2, 24.03.2008, p. 61-71.Research output: Contribution to journal › Article
}
TY - JOUR
T1 - Coupling among pitch motion, axial vibration, and orbital motion of large space structures
AU - Ishimura, Kosei
AU - Higuchi, Ken
PY - 2008/3/24
Y1 - 2008/3/24
N2 - The parameter dependency of large space structures on the coupling among attitude motion, structural vibration, and orbital motion has been investigated, particularly for structures such as tethered satellite systems. Tethered satellites are noticed for their possible applications. From space solar power systems to deorbit system, the applications of tethered satellites spread out over various fields. In this paper, we investigate planar motion of a satellite model, which consists of two tip particles and a massless spring. For such a space structure, the characteristics of the planar motion are shown to be determined by the mass ratio of tip particles, the natural frequency ratio of axial vibration to orbital motion, and the axial length ratio of the spring to the orbital radius. Among these three parameters, the natural frequency ratio has the greatest influence on the coupling phenomenon. Furthermore, the parameter range over which the coupling phenomenon occurs is specified.
AB - The parameter dependency of large space structures on the coupling among attitude motion, structural vibration, and orbital motion has been investigated, particularly for structures such as tethered satellite systems. Tethered satellites are noticed for their possible applications. From space solar power systems to deorbit system, the applications of tethered satellites spread out over various fields. In this paper, we investigate planar motion of a satellite model, which consists of two tip particles and a massless spring. For such a space structure, the characteristics of the planar motion are shown to be determined by the mass ratio of tip particles, the natural frequency ratio of axial vibration to orbital motion, and the axial length ratio of the spring to the orbital radius. Among these three parameters, the natural frequency ratio has the greatest influence on the coupling phenomenon. Furthermore, the parameter range over which the coupling phenomenon occurs is specified.
KW - Aerospace engineering
KW - Space structures
KW - Structural dynamics
KW - Vibration
UR - http://www.scopus.com/inward/record.url?scp=40849083755&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=40849083755&partnerID=8YFLogxK
U2 - 10.1061/(ASCE)0893-1321(2008)21:2(61)
DO - 10.1061/(ASCE)0893-1321(2008)21:2(61)
M3 - Article
VL - 21
SP - 61
EP - 71
JO - Journal of Aerospace Engineering
JF - Journal of Aerospace Engineering
SN - 0893-1321
IS - 2
ER -