Abstract
This paper discusses a position and attitude control problem of an underactuated satellite which uses on-off thruster mechanisms for control. Each thrusters has constant orientation relative to the satellite's body, and can generate only unilateral forces. The purpose of this paper is to clarify the control law for simultaneous position and attitude control for this type of satellite configuration. Considering the input constraints, we obtain the analytical solutions of the satellite's translational and rotational motion. Then the control procedure utilizing an invariant manifold is derived. Some numerical simulations are shown to verify the effectiveness of the proposed controller.
| Original language | English |
|---|---|
| Title of host publication | AIAA Guidance, Navigation, and Control Conference 2011 |
| Publication status | Published - 2011 |
| Event | AIAA Guidance, Navigation and Control Conference 2011 - Portland, OR, United States Duration: Aug 8 2011 → Aug 11 2011 |
Other
| Other | AIAA Guidance, Navigation and Control Conference 2011 |
|---|---|
| Country | United States |
| City | Portland, OR |
| Period | 8/8/11 → 8/11/11 |
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All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Control and Systems Engineering
- Electrical and Electronic Engineering
Cite this
Position and attitude control of an underactuated satellite with constant thrust. / Yoshimura, Yasuhiro; Matsuno, Takashi; Hokamoto, Shinji.
AIAA Guidance, Navigation, and Control Conference 2011. 2011.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
}
TY - GEN
T1 - Position and attitude control of an underactuated satellite with constant thrust
AU - Yoshimura, Yasuhiro
AU - Matsuno, Takashi
AU - Hokamoto, Shinji
PY - 2011
Y1 - 2011
N2 - This paper discusses a position and attitude control problem of an underactuated satellite which uses on-off thruster mechanisms for control. Each thrusters has constant orientation relative to the satellite's body, and can generate only unilateral forces. The purpose of this paper is to clarify the control law for simultaneous position and attitude control for this type of satellite configuration. Considering the input constraints, we obtain the analytical solutions of the satellite's translational and rotational motion. Then the control procedure utilizing an invariant manifold is derived. Some numerical simulations are shown to verify the effectiveness of the proposed controller.
AB - This paper discusses a position and attitude control problem of an underactuated satellite which uses on-off thruster mechanisms for control. Each thrusters has constant orientation relative to the satellite's body, and can generate only unilateral forces. The purpose of this paper is to clarify the control law for simultaneous position and attitude control for this type of satellite configuration. Considering the input constraints, we obtain the analytical solutions of the satellite's translational and rotational motion. Then the control procedure utilizing an invariant manifold is derived. Some numerical simulations are shown to verify the effectiveness of the proposed controller.
UR - http://www.scopus.com/inward/record.url?scp=84878713745&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84878713745&partnerID=8YFLogxK
M3 - Conference contribution
SN - 9781600869525
BT - AIAA Guidance, Navigation, and Control Conference 2011
ER -