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The use of the articulated total body model as a robot dynamics simulation toolThe Articulated Total Body (ATB) model is a computer sumulation program which was originally developed for the study of aircrew member dynamics during ejection from high-speed aircraft. This model is totally three-dimensional and is based on the rigid body dynamics of coupled systems which use Euler's equations of motion with constraint relations of the type employed in the Lagrange method. In this paper the use of the ATB model as a robot dynamics simulation tool is discussed and various simulations are demonstrated. For this purpose the ATB model has been modified to allow for the application of torques at the joints as functions of state variables of the system. Specifically, the motion of a robotic arm with six revolute articulations with joint torques prescribed as functions of angular displacement and angular velocity are demonstrated. The simulation procedures developed in this work may serve as valuable tools for analyzing robotic mechanisms, dynamic effects, joint load transmissions, feed-back control algorithms employed in the actuator control and end-effector trajectories.
Document ID
19890010501
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Obergfell, Louise A.
(Aerospace Medical Research Labs. Wright-Patterson AFB, OH, United States)
Avula, Xavier J. R.
(Aerospace Medical Research Labs. Wright-Patterson AFB, OH, United States)
Kalegs, Ints
(Aerospace Medical Research Labs. Wright-Patterson AFB, OH, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1988
Publication Information
Publication: NASA. Lyndon B. Johnson Space Center, 2nd Annual Workshop on Space Operations Automation and Robotics (SOAR 1988)
Subject Category
Man/System Technology And Life Support
Accession Number
89N19872
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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