Abstract
This paper presents a new ground-based satellite formation ying testbed. Mainly consisting of multiple five-degrees-of-freedom (DOF) satellite motion simulators, at table, and tracking system, Autonomous Satellite Test Environment for Rendezvous In proXimity (ASTERIX) facility is designed to test and validate novel relative guidance, navigation, and control (GNC) algorithms for satellite formation ying missions. Imitating a member in formation, each satellite motion simulator works in group to demonstrate and validate advanced space technology such as proximity operations, autonomous rendezvous and docking (ARD), collision avoidance, etc. This work shows up-to-date development status of the new testbed regarding the prototype configuration, integration, and experimental results. Design improvements and changes in operation strategies is discussed for the final design based on structural and functional analysis using the pre-developed prototype. Preliminary experimental results on the performance analysis of equipments such as continuous thrust generation using proportional solenoid valves and attitude maneuver using reaction wheel assembly (RWA) is also presented.
| Original language | English |
|---|---|
| Title of host publication | AIAA Modeling and Simulation Technologies Conference |
| Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
| ISBN (Print) | 9781624103872 |
| Publication status | Published - 2016 Jan 1 |
| Event | AIAA Modeling and Simulation Technologies Conference, 2016 - San Diego, United States Duration: 2016 Jan 4 → 2016 Jan 8 |
Other
| Other | AIAA Modeling and Simulation Technologies Conference, 2016 |
|---|---|
| Country | United States |
| City | San Diego |
| Period | 16/1/4 → 16/1/8 |
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All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Modelling and Simulation
Cite this
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Design and development of ground-based 5-DOF satellite formation flying testbed. / Eun, Youngho; Park, Chandeok; Park, Sang Young.
AIAA Modeling and Simulation Technologies Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, 2016.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
TY - GEN
T1 - Design and development of ground-based 5-DOF satellite formation flying testbed
AU - Eun, Youngho
AU - Park, Chandeok
AU - Park, Sang Young
PY - 2016/1/1
Y1 - 2016/1/1
N2 - This paper presents a new ground-based satellite formation ying testbed. Mainly consisting of multiple five-degrees-of-freedom (DOF) satellite motion simulators, at table, and tracking system, Autonomous Satellite Test Environment for Rendezvous In proXimity (ASTERIX) facility is designed to test and validate novel relative guidance, navigation, and control (GNC) algorithms for satellite formation ying missions. Imitating a member in formation, each satellite motion simulator works in group to demonstrate and validate advanced space technology such as proximity operations, autonomous rendezvous and docking (ARD), collision avoidance, etc. This work shows up-to-date development status of the new testbed regarding the prototype configuration, integration, and experimental results. Design improvements and changes in operation strategies is discussed for the final design based on structural and functional analysis using the pre-developed prototype. Preliminary experimental results on the performance analysis of equipments such as continuous thrust generation using proportional solenoid valves and attitude maneuver using reaction wheel assembly (RWA) is also presented.
AB - This paper presents a new ground-based satellite formation ying testbed. Mainly consisting of multiple five-degrees-of-freedom (DOF) satellite motion simulators, at table, and tracking system, Autonomous Satellite Test Environment for Rendezvous In proXimity (ASTERIX) facility is designed to test and validate novel relative guidance, navigation, and control (GNC) algorithms for satellite formation ying missions. Imitating a member in formation, each satellite motion simulator works in group to demonstrate and validate advanced space technology such as proximity operations, autonomous rendezvous and docking (ARD), collision avoidance, etc. This work shows up-to-date development status of the new testbed regarding the prototype configuration, integration, and experimental results. Design improvements and changes in operation strategies is discussed for the final design based on structural and functional analysis using the pre-developed prototype. Preliminary experimental results on the performance analysis of equipments such as continuous thrust generation using proportional solenoid valves and attitude maneuver using reaction wheel assembly (RWA) is also presented.
UR - http://www.scopus.com/inward/record.url?scp=84957999160&partnerID=8YFLogxK
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M3 - Conference contribution
SN - 9781624103872
BT - AIAA Modeling and Simulation Technologies Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
ER -