TY - JOUR
T1 - Coordinated Control of a Dual-Arm Space Robot
T2 - Novel Models and Simulations for Robotic Control Methods
AU - Shi, Lingling
AU - Jayakody, Hiranya
AU - Katupitiya, Jayantha
AU - Jin, Xin
N1 - Publisher Copyright:
© 1994-2011 IEEE.
PY - 2018/12
Y1 - 2018/12
N2 - Space robots have attracted increasing attention for performing, autonomously or telerobotically, on-orbit servicing missions such as repairing, refueling, and upgrading spacecraft; reusing space assets; and on-orbit assembly. The extension of robot application to space can release astronauts from risky, time-consuming, and expensive extravehicular activities [1]. However, in the microgravity environment, the floating base of a space robot will be disturbed by the robot's arm motion when it approaches or manipulates a target. The motion of the spacecraft base resulting from this disturbance will, conversely, affect the motion of end effectors (known as coupling dynamics), making control of space robots more complicated than that of fixed-base robots. In addition, such a disturbance of spacecraft attitude may result in a communication interruption between the spacecraft and the ground station or a failure of energy accumulation caused by disorientation of solar panels [2].
AB - Space robots have attracted increasing attention for performing, autonomously or telerobotically, on-orbit servicing missions such as repairing, refueling, and upgrading spacecraft; reusing space assets; and on-orbit assembly. The extension of robot application to space can release astronauts from risky, time-consuming, and expensive extravehicular activities [1]. However, in the microgravity environment, the floating base of a space robot will be disturbed by the robot's arm motion when it approaches or manipulates a target. The motion of the spacecraft base resulting from this disturbance will, conversely, affect the motion of end effectors (known as coupling dynamics), making control of space robots more complicated than that of fixed-base robots. In addition, such a disturbance of spacecraft attitude may result in a communication interruption between the spacecraft and the ground station or a failure of energy accumulation caused by disorientation of solar panels [2].
UR - http://www.scopus.com/inward/record.url?scp=85054356825&partnerID=8YFLogxK
U2 - 10.1109/MRA.2018.2864717
DO - 10.1109/MRA.2018.2864717
M3 - Article
AN - SCOPUS:85054356825
SN - 1070-9932
VL - 25
SP - 86
EP - 95
JO - IEEE Robotics and Automation Magazine
JF - IEEE Robotics and Automation Magazine
IS - 4
M1 - 8472216
ER -