Biomedical Engineering Reference
In-Depth Information
principle of virtual work to the two force systems. As for the joint torques, its
associated virtual work is
T
δ
W τ 5 τ
δ
q
(4.4)
T
where
δ
W is the virtual work and
τ
denotes the transpose of
τ
. For the
T , comprised of a force vector f and a moment
vector m, the virtual work performed is
δ
5 ½ f T
m T
end-effector forces F
W F 5 f T
δ x 1 m T
ωδ
t
(4.5)
where
t is the angular virtual displace-
ment of the end-effector, respectively. Because the difference between the virtual
work of the joint torques and the virtual work of the end-effector forces shall be
null for all joint virtual displacements, we write
δ x is the linear virtual displacement and
ωδ
T
F T J ð q Þδ
τ
δ
q
q
q
(4.6)
5
'
The relationship between the joint
torque vector and end-effector force/
moment vector is then given by
J T F
τ 5
(4.7)
T .
Now, we extend this formulation to the case where multiple external loads
(both translational and rotational) are applied to any location of any link, not nec-
essarily to the end-effector. Let's assume that a general form of external load F k
is applied to the point at
τ 5 ½τ 1 ; τ 2 ; ...; τ n
where the torque vector is
k r k location of link k, where
k r k location vector is
expressed with respect to k th local coordinate frame.
This point of application of external load can be regarded as the end-effector
for the corresponding external load. The augmented Jacobian matrix J k for this
point is derived from the linear relationship between the joint velocity vector and
the Cartesian velocity vector:
2
3
0 T 1 ð q Þ
@
0 T i ð q Þ
@
0 T k ð q Þ
@
@
@
@
k r k
k r k
k r k
...
...
4
5 6 3 k
J k ð q Þ 5
q 1
q i
q k
(4.8)
Z 0 ð q Þ
...
Z i 2 1 ð q Þ
...
Z k 2 1 ð q Þ
where, i
k is the local z-axis vector of joint i expressed in terms of the
global coordinate system.
Therefore the joint torque vector due to the external load applied at point
1
; ...;
5
k r k
of link k is
J k F k (4.9)
From the principle of superposition, the total joint torques due to several
external loads is obtained as a sum of all joint torques:
τ k 5
X
J k F k
τ 5
(4.10)
k
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