Abstract
This paper studies a control law to stabilize the orbital motion in the vicinity of an unstable equilibrium points and periodic orbits in the circular-restricted three-body problem. Utilizing the eigenstructure of the system, the fuel efficient formation flying controller via linear quadratic regulator (LQR) is developed. Then the chattering attenuation sliding mode controller (CASMC) is designed and analyzed for the in-plane motion of the circular circular-restricted three-body problem. Simulation studies are conducted for the Sun-Earth L2 point and a halo orbit around it. The total velocity change required to reach the halo orbit as well as to maintain the halo orbit is calculated. Simulation results show that the chattering attenuation sliding mode controller has good performance and robustness in the presence of unmodeled nonlinearity along the halo orbit with relatively small fuel consumption.
| Original language | English |
|---|---|
| Title of host publication | Astrodynamics 2015 |
| Editors | James D. Turner, Geoff G. Wawrzyniak, William Todd Cerven, Manoranjan Majji |
| Publisher | Univelt Inc. |
| Pages | 785-804 |
| Number of pages | 20 |
| ISBN (Print) | 9780877036296 |
| Publication status | Published - Jan 1 2016 |
| Event | AAS/AIAA Astrodynamics Specialist Conference, ASC 2015 - Vail, United States Duration: Aug 9 2015 → Aug 13 2015 |
Publication series
| Name | Advances in the Astronautical Sciences |
|---|---|
| Volume | 156 |
| ISSN (Print) | 0065-3438 |
Other
| Other | AAS/AIAA Astrodynamics Specialist Conference, ASC 2015 |
|---|---|
| Country | United States |
| City | Vail |
| Period | 8/9/15 → 8/13/15 |
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All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Space and Planetary Science
Cite this
Satellite formation-keeping about libration points in the presence of system uncertainties. / Bando, Mai; Nemati, Hamidreza; Hokamoto, Shinji.
Astrodynamics 2015. ed. / James D. Turner; Geoff G. Wawrzyniak; William Todd Cerven; Manoranjan Majji. Univelt Inc., 2016. p. 785-804 (Advances in the Astronautical Sciences; Vol. 156).Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
}
TY - GEN
T1 - Satellite formation-keeping about libration points in the presence of system uncertainties
AU - Bando, Mai
AU - Nemati, Hamidreza
AU - Hokamoto, Shinji
PY - 2016/1/1
Y1 - 2016/1/1
N2 - This paper studies a control law to stabilize the orbital motion in the vicinity of an unstable equilibrium points and periodic orbits in the circular-restricted three-body problem. Utilizing the eigenstructure of the system, the fuel efficient formation flying controller via linear quadratic regulator (LQR) is developed. Then the chattering attenuation sliding mode controller (CASMC) is designed and analyzed for the in-plane motion of the circular circular-restricted three-body problem. Simulation studies are conducted for the Sun-Earth L2 point and a halo orbit around it. The total velocity change required to reach the halo orbit as well as to maintain the halo orbit is calculated. Simulation results show that the chattering attenuation sliding mode controller has good performance and robustness in the presence of unmodeled nonlinearity along the halo orbit with relatively small fuel consumption.
AB - This paper studies a control law to stabilize the orbital motion in the vicinity of an unstable equilibrium points and periodic orbits in the circular-restricted three-body problem. Utilizing the eigenstructure of the system, the fuel efficient formation flying controller via linear quadratic regulator (LQR) is developed. Then the chattering attenuation sliding mode controller (CASMC) is designed and analyzed for the in-plane motion of the circular circular-restricted three-body problem. Simulation studies are conducted for the Sun-Earth L2 point and a halo orbit around it. The total velocity change required to reach the halo orbit as well as to maintain the halo orbit is calculated. Simulation results show that the chattering attenuation sliding mode controller has good performance and robustness in the presence of unmodeled nonlinearity along the halo orbit with relatively small fuel consumption.
UR - http://www.scopus.com/inward/record.url?scp=85007290806&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85007290806&partnerID=8YFLogxK
M3 - Conference contribution
SN - 9780877036296
T3 - Advances in the Astronautical Sciences
SP - 785
EP - 804
BT - Astrodynamics 2015
A2 - Turner, James D.
A2 - Wawrzyniak, Geoff G.
A2 - Cerven, William Todd
A2 - Majji, Manoranjan
PB - Univelt Inc.
ER -