IEEE - Aerospace and Electronic Systems - January 2022 - 34

Microgravity Performance Evaluation for Zero Gravity Robot in China's Space Station
gas of the air-jet thrusters comes from a gas storage cylinder,
which can support the air-jet thrusters working continuously
for no less than one hour and can be reinflated. The electromagnetic
actuators consist ofpermanent magnets fixed on the
inner body and two sets oforthogonal coils fixed on the outer
body, which can generate force in two DOF.
The electric unit mounted on the outer body is used for
calculations related to the motion control ofthe inner body
and the outer body, as well as the reception and transmission
of instructions and data. The energy components
include some lithium batteries mounted on the outer body
and a wireless energy transfer device placed between the
inner body and the outer body. The lithium batteries supply
power to the outer body directly and supply power to
the inner body through wireless transmission. The communication
components include two sets of wireless-fidelity
components mounted on the inner body and the outer
body, and one set of infrared transceiver module placed
between them.
The sensors and actuators of ZGR is listed in Table I.
The frequency responses of the sensors are the measurement
frequencies, and the frequency responses of the
actuators are the output frequencies.
Figure 3.
Main components ofZGR.
accelerometers are used for high-accuracy measurement
of microgravity acceleration of the inner body. The 2DPSDs
measure the relative motion between the inner body
and the outer body.
The actuators include 24 air-jet thrusters mounted on
the outer body and three sets of electromagnetic actuators
placed between the inner body and the outer body. The
Table 1.
Sensors and Actuators of ZGR
Component
Sensor Cameras
MEMS
Three-axis electrostatic-levitation
accelerometers
2D-PSDs
Actuator Air-jet thrusters
Electromagnetic actuators
WORKING MODES
There are three working modes for ZGR, including an outside-rack
air-suspension mode, an inside-rack air-suspension
mode, and an inside-rack magnetic-levitation mode.
The outside-rack air-suspension mode is designed to operate
ZGR out ofHMLR (directly inside TH) under the spatial
constraints of500 mm and10. The inside-rack
air-suspension mode is designed to operate ZGR by the
air-jet thrusters and electromagnetic actuators in HMLR
Frequency
response
Accuracy
10 Hz
50 Hz
20 Hz
100 Hz
4 Hz
50 Hz
0.59 mm and 0.07 inside the rack
5.15 mm and 0.23 outside the rack
0.25/h and 1.910-5 m/s2
110-6-510-7 m/s2/Hz1/2 @
0.01-0.1 Hz
510-7-510-6 m/s2/Hz1/2 @ 0.1-5 Hz
50 mm (measurement accuracy of
spot position)
50 mN
1%-1% (relative accuracy) @
5 mN-5 N
34
IEEE A&E SYSTEMS MAGAZINE
JANUARY 2022

IEEE - Aerospace and Electronic Systems - January 2022

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