Caption: The calculation of center of mass illustrated.
Features:
The result is the center of mass---more explicitly the center-of-mass position vector.
R_cm = ∑_i (m_i*R_i) / ∑_i (m_i) = sum;_i (m_i*R_i) / mwhere capital letters signify vectors, R_cm is the center of mass, i is an index for the bits, R_i is the position vector for bit i, m_i is the mass of bit i, and m is the system mass (i.e., the total mass).
F_net_ext = m*A_cm ,where F_net_ext is the net external force on the system, m is again the system mass, and A_cm is the center-of-mass acceleration.
So it's center-of-mass motion which is determined by F=ma---a point often neglected in high-school physics courses.
Center-of-mass (CM)
inertial frames
are discussed in file Mechanics file:
frame_basics.html.
Their special cases,
celestial frames
and comoving frames
are discussed in file Mechanics file:
frame_hierarchy_astro.html.
where
"sub" stands for subsystem,
R_sub_cm is the center of mass
evaluated using the subsystem centers of mass,
R_cm is the center of mass evaluated
from the elementary particles (i.e., the true
center of mass of the
system),
the index i labels the subsystems,
R_sub_i is the center of mass of
subsystem i,
m_sub_i is the mass of
subsystem i,
the index ij labels elementary particles in subsytem i
(and thus their
masses
and position vectors),
and k labels elementary particles in general
(and thus their
masses
and position vectors).
The division into subsystems is general and the division into elementary particles
is unique in some mythical limiting sense yours truly hopes.
m*R_sub_cm = ∑_i ( m_sub_i*R_sub_i ) = ∑_i ∑_j ( m_ij*R_ij )
= ∑_k (m_k*R_k) = m*R_cm ,
and thus vec_R_sub_cm = vec_R_cm,
QED.