Abstract
This paper deals with the two-dimensional position and attitude control of a satellite by on-off thrusters which are fixed to the satellite's body. Since the thrusters generate constant and unilateral forces, the equations of motion form nonholonomic constraint and cannot be integrated. Furthermore, the satellite's mass changes due to the fuel consumption. Utilizing Fresnel integrals and the partial integrals, we derive the approximate analytic solution considering the satellite's mass change to achieve a specified satellite's position and attitude. The accuracy of the proposed approximate technique is verified by applying it to a condition considered in SLIM project of JAXA.
| Original language | English |
|---|---|
| Title of host publication | ASTRODYNAMICS 2011 - Advances in the Astronautical Sciences |
| Subtitle of host publication | Proceedings of the AAS/AIAA Astrodynamics Specialist Conference |
| Pages | 2953-2964 |
| Number of pages | 12 |
| Volume | 142 |
| Publication status | Published - 2012 |
| Event | 2011 AAS/AIAA Astrodynamics Specialist Conference, ASTRODYNAMICS 2011 - Girdwood, AK, United States Duration: Jul 31 2011 → Aug 4 2011 |
Other
| Other | 2011 AAS/AIAA Astrodynamics Specialist Conference, ASTRODYNAMICS 2011 |
|---|---|
| Country | United States |
| City | Girdwood, AK |
| Period | 7/31/11 → 8/4/11 |
Fingerprint
All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Space and Planetary Science
Cite this
Satellite position and attitude control by on-off thrusters considering mass change. / Yoshimura, Yasuhiro; Matsuno, Takashi; Hokamoto, Shinji.
ASTRODYNAMICS 2011 - Advances in the Astronautical Sciences: Proceedings of the AAS/AIAA Astrodynamics Specialist Conference. Vol. 142 2012. p. 2953-2964.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
}
TY - GEN
T1 - Satellite position and attitude control by on-off thrusters considering mass change
AU - Yoshimura, Yasuhiro
AU - Matsuno, Takashi
AU - Hokamoto, Shinji
PY - 2012
Y1 - 2012
N2 - This paper deals with the two-dimensional position and attitude control of a satellite by on-off thrusters which are fixed to the satellite's body. Since the thrusters generate constant and unilateral forces, the equations of motion form nonholonomic constraint and cannot be integrated. Furthermore, the satellite's mass changes due to the fuel consumption. Utilizing Fresnel integrals and the partial integrals, we derive the approximate analytic solution considering the satellite's mass change to achieve a specified satellite's position and attitude. The accuracy of the proposed approximate technique is verified by applying it to a condition considered in SLIM project of JAXA.
AB - This paper deals with the two-dimensional position and attitude control of a satellite by on-off thrusters which are fixed to the satellite's body. Since the thrusters generate constant and unilateral forces, the equations of motion form nonholonomic constraint and cannot be integrated. Furthermore, the satellite's mass changes due to the fuel consumption. Utilizing Fresnel integrals and the partial integrals, we derive the approximate analytic solution considering the satellite's mass change to achieve a specified satellite's position and attitude. The accuracy of the proposed approximate technique is verified by applying it to a condition considered in SLIM project of JAXA.
UR - http://www.scopus.com/inward/record.url?scp=84877945215&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84877945215&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84877945215
SN - 9780877035770
VL - 142
SP - 2953
EP - 2964
BT - ASTRODYNAMICS 2011 - Advances in the Astronautical Sciences
ER -