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Introduction to Sports Biomechanics: Analysing Human Movement ...

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INTRODUCTION TO SPORTS BIOMECHANICS<br />

192<br />

inertia through the centre of mass correspond with the three cardinal axes. The moment<br />

of inertia about the vertical axis is much smaller – about one-tenth – of the moment of<br />

inertia about the other two axes and that about the frontal axis is slightly less than that<br />

about the sagittal axis. It is worth noting that rotations about the intermediate principal<br />

axis, here the frontal axis, are unstable, whereas those about the principal axes with the<br />

greatest and smallest moments of inertia are stable. This is another fac<strong>to</strong>r making layout<br />

somersaults difficult, unless the body is realigned <strong>to</strong> make the moment of inertia about<br />

the frontal, or somersault, axis greater than that about the sagittal axis.<br />

For the sports performer, movements of the limbs other than in symmetry away<br />

from the ana<strong>to</strong>mical reference position result in a misalignment between the body’s<br />

cardinal axes and the principal axes of inertia. This has important consequences for the<br />

generation of aerial twist in a twisting somersault.<br />

BOX 5.3 LAWS OF ANGULAR MOTION<br />

The laws of angular motion are analogous <strong>to</strong> New<strong>to</strong>n’s three laws of linear motion.<br />

Principle of conservation of angular momentum (law of inertia)<br />

A rotating body will continue <strong>to</strong> turn about its axis of rotation with constant angular momentum<br />

unless an external <strong>to</strong>rque (moment of force) acts on it. The magnitude of the <strong>to</strong>rque about an axis<br />

of rotation is the product of the force and its moment arm, which is the perpendicular distance<br />

from the axis of rotation <strong>to</strong> the line of action of the force.<br />

Law of momentum<br />

The rate of change with time (d/dt) of angular momentum (L) of a body is proportional <strong>to</strong> the<br />

<strong>to</strong>rque (M) causing it and has the same direction as the <strong>to</strong>rque. This is expressed symbolically by<br />

the following equation, which holds true for rotation about any axis fixed in space: M = dL/dt. If<br />

we now rearrange this equation by multiplying by dt, and integrate it, we obtain: ∫M dt = ∫dL =<br />

∆L; that is, the impulse of the <strong>to</strong>rque equals the change of angular momentum (∆L). If the <strong>to</strong>rque<br />

impulse is zero, this equation reduces <strong>to</strong>: ∆L = 0 or L = constant, which is a mathematical<br />

statement of the first law of angular motion.<br />

The last equation in the previous paragraph can be modified by writing L = I ω where I is the<br />

moment of inertia and ω is the angular velocity of the body if, and only if, the axis of rotation<br />

is fixed in space or is a principal axis of inertia of a rigid or quasi-rigid body. Then, and only then,<br />

M = d(I ω)/dt. Furthermore if, and only if, I is constant (for example for an individual rigid or<br />

quasi-rigid body segment): M = I α, where α is the angular acceleration. The restrictions on the use<br />

of the equations in this paragraph compared with the universality of the equations in the previous<br />

paragraph should be carefully noted.<br />

The angular motion equations for three-dimensional rotation are far more complex than the<br />

ones above and will not be considered in this book.

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