Dynamics 2e 25
Problem 1.20
To study the motion of a space station, the station can be modeled as a rigid
body and the equations describing its motion can be chosen to be Euler’s
equations, which read
MxDIxx ˛xIyy I´´!y!´;
MyDIyy ˛yI´´ Ixx!x!´;
M´DI´´ ˛´Ixx Iyy !x!y:
In the previous equations,
Mx
,
My
, and
M´
denote the
x
,
y
, and
´
com-
ponents of the moment applied to the body;
!x
,
!y
, and
!´
denote the
corresponding components of the angular velocity of the body, where angu-
lar velocity is defined as the time rate of change of an angle;
˛x
,
˛y
, and
˛´
denote the corresponding components of the angular acceleration of the
body, where angular acceleration is defined as the time rate of change of an
angular velocity. The quantities
Ixx
,
Iyy
, and
I´´
are called the principal
mass moments of inertia of the body. Determine the dimensions of
Ixx
,
Iyy
,
and
I´´
and determine their units in SI, as well as in the U.S. Customary
system.
Solution
Let
L
,
M
, and
T
denote length, mass, and time, respectively. We consider only one of the three equations as
their dimensions are identical:
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