@InProceedings{FonsecaLimaSaotOliv:2018:SpRoDy,
author = "Fonseca, Ijar da and Lima, Glaydson L. B. and Saotome, Osamu and
Oliveira, {\'E}lcio Jeronimo de",
affiliation = "{Instituto Tecnologico de Aeron{\'a}utica (ITA)} and {Instituto
Tecnologico de Aeron{\'a}utica (ITA)} and {Instituto Tecnologico
de Aeron{\'a}utica (ITA)} and {Instituto Nacional de Pesquisas
Espaciais (INPE)}",
title = "Space robot dynamic analysis of the relative orbital and attitude
motion in the close range rendezvous phase and grasping of a
target space vehicle",
year = "2018",
organization = "International Astronautical Congress, 69.",
abstract = "This article deals with the dynamic analysis of the close approach
phase of a space robot to a target spacecraft aiming the grasping
of a target space vehicle. The chaser robot shall berth by side of
the target so as to have it inside its workspace envelop. The
grasping operation shall be executed by inverse kinematics. The
computer simulation of the equations of the dynamics (relative
orbital and attitude equations of motion) yields the grasping
conditions and such results are compared with the inverse
kinematics grasping operation implemented in a lab experiment. In
the experiment it is used two robot manipulators mounted on an air
supported platform, constituting a floating robotic system that
operates on a glass table. The experiment is wireless and this
feature is obtained by using Wifi to implement the communication
of the human operator with the robots and a platform containing
its own air compressed cylinders. In addition to the Wifi the
manipulator platforms include microcontroller, a set of valves to
control the compressed air flow, and two compressed air cylinders.
The actuators for rotational/translational motion operate on the
base of compressed air. A Kinect v2 sensor supported by
computational vision is employed externally to the experiment. The
use of such sensor aims to measure velocity, perform robot
tracking as well as to obtain the X, Y, and Z positions of the
manipulators grippers at run time and 3D video scenes. The
information is sent via Wifi, over the UDP protocol, to a computer
with MATLAB software, which writes the actual speed and
positioning information and compares with the prescribed results
(estimated in simulation). The experimental result obtained by
inverse kinematics for the capture of the target is compared with
the results of the computational simulations, aiming at the
validation and improvement of the mathematical model simulated via
MATLAB. If the error does not meet the nominal specification the
operator commands the robot system to continue the control loop.
The compressed air autonomy is about 30 minutes for the platform
floating and 1 minute for the grasping operation. The results are
presented by using plots of the relative distance and velocity
with respect to time, attitude synchronization with respect to
time, and the robot-like spacecraft attitude motion during the
safety-critical operations of grasping the target spacecraft. The
direct kinematics obtained by the computational simulation is
compared with the results of the inverse kinematics obtained via
experiment.",
conference-location = "Bremen",
conference-year = "01-05 oct.",
language = "pt",
urlaccessdate = "28 abr. 2024"
}