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W. Richard Bowen and Nidal Hilal 4

W. Richard Bowen and Nidal Hilal 4

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8 1. BAsIC PRINCIPLEs OF ATOMIC FORCE MICROsCOPy<br />

where M is the added mass, k the cantilever spring constant <strong>and</strong> v 0 <strong>and</strong> v 1<br />

the unloaded <strong>and</strong> loaded resonant frequencies.<br />

Although this method can produce a value for the cantilever<br />

spring constant to a high degree of accuracy, there are some problems.<br />

Attaching the bead to the cantilever, especially if attached using glue,<br />

can be a destructive process, rendering the lever unusable for further<br />

experiments. This means that calibration must be carried out at the end<br />

of experimental measurements. However, with sufficient care spheres<br />

may be attached in air using capillary adhesion forces alone. In addition<br />

errors may occur from the incorrect placement of the sphere or uncertainties<br />

in the mass of the sphere. If the sphere is placed a short distance<br />

away from the end of the lever, then the value obtained from this<br />

method will be high, as k is inversely proportional to the cube of the<br />

cantilever length l. Again, this can be simply accounted for by utilizing<br />

equation (1.4).<br />

The masses of spheres ordinarily used in this technique are on the<br />

order of a nanogram, making accurate weighing problematic. As such,<br />

masses are generally estimated from the size <strong>and</strong> density of the spheres,<br />

which may in turn lead to measurement errors. To allow for this, measurements<br />

may be made using several spheres of different masses. A plot of M<br />

versus (2�v 1) �2 can then be made, which will have a slope equal to the<br />

spring constant of the cantilever [95, 101]. The advantages of this method<br />

are that the measurements are independent of the cantilever geometry<br />

<strong>and</strong> material properties, <strong>and</strong> many commercially available AFMs have the<br />

capability to measure cantilever resonant frequencies.<br />

Another technique commonly used to quantify cantilever spring<br />

constants is the so-called ‘thermal method’ devised by Hutter <strong>and</strong><br />

Bechhoefer [102, 103]. Here the area of the fundamental resonant peak<br />

of the cantilever under ambient thermal excitation, when not in the presence<br />

of a surface, can be used to directly calculate the spring constant of<br />

the cantilever. The mean square deflection of the cantilever, x 2 , due to<br />

thermal fluctuations can be related to the spring constant thus, assuming<br />

an idealised spring behaviour:<br />

kBT k �<br />

2<br />

x<br />

(1.7)<br />

where k B <strong>and</strong> T are Boltzmann’s constant (1.38 � 10 �23 J K �1 ) <strong>and</strong> absolute<br />

temperature, respectively, together representing the thermal energy<br />

of the system. Once other noise sources are subtracted from the background,<br />

the area of the fundamental resonance peak will be equal to the<br />

mean square displacement. However, as the cantilever is not an ideal

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