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68 Brooks believes that we are now about to leave behind the ideological battles of the 1930s, 1960s, and 1990s He believes we may be entering a more pragmatic, more analytical decade or two Convinced.

To be able to optimize the source program code, the optimizer performs control ow analysis and data ow analysis of the program and of each basic block. It constructs control ow and data ow graphs in some forms, speci c for the optimizer, that specify control and data dependencies between the elements of the program. Here are the most important kinds of such dependencies [13]. The statement S2 is control dependent on the statement S1 if the execution of S2 depends on the conditions evaluated in S1. For example: S1 S2 S3 if i > 0 then goto L1; a := 1; L1: c := a + 2;

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side with the attendant unwanted heat generation. This deadband, however, can be a problem to the control system designer because the ow gain of the valve is zero within the range of the deadband. The curve in the ow line is caused by the circular ports in the valve sleeve that produce a nonlinear ow area as the valve is moved away from the null position. This nonlinearity can be avoided by cutting rectangular ports in the sleeve which is a commonly used but more expensive process. The third nonlinearity shown on this graph is the saturation feature that represents the effect of having a ow limiter in the hydraulic supply line or a travel limit designed into the error linkage. The above example serves to demonstrate that both forms of nonlinearity can (and often do) occur together and that this must be borne in mind when analyzing complex systems. The two forms of nonlinearity will now be addressed separately using common real world examples as a basis for discussion and explanation. There is one additional form of nonlinearity that must be mentioned here and that is the pure time delay also referred to as a transport delay or dead time. This type of nonlinearity falls into neither of the above two categories and will therefore be discussed as a separate topic.

The Surface modifier is the other part of the surface tools. It creates a surface from several combined splines. It can use any spline network but works best with structures created with the CrossSection modifier. The surface created with this modifier is a patch surface. Parameters for this modifier include a Spline Threshold value and options to Flip Normals, Remove Interior Patches, and Use Only Selected Segments. You can also specify the steps used to create the patch topology. After the surface is created, you can apply the Edit Patch modifier to further edit and refine the patch surface.

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Analog electronic controls in aircraft applications were enabled largely by the advent of the transistor and solid state electronics technology. During the 1960s and 1970s before the availability of general purpose single chip microprocessors, the control system designer looked rst to analog electronics technology to provide an easy way to implement custom dynamic functions. We saw the introduction of auto-stabilizers in ight control systems providing limited authority trim functions that added to the pilots mechanical commands. Engine controls saw the introduction of the supervisory control as a means to reduce pilot workload and to enhance the maintenance intervals by preventing inadvertent exceedances such as transient over-temperature events that can seriously reduce the engine hot section life. Two of the most ambitious accomplishments of analog control technology developed in the 1960s were the rst aircraft Auto-land system developed by Smiths Industries and the quadruplex ight control system for the USAF F-16 aircraft developed and produced by the Astronics Division of Lear Seigler. These analog control systems were eventually replaced by digital electronic controls. As the growth in electronic technology continued there emerged an increase in the application of hybrid electronics technology wherein analog electronics was mixed in with the emerging digital technology. This was a stepping stone towards the application of custom digital computer designs later developed by the large corporations who were prepared to absorb the expensive tooling costs associated with custom electronics in an attempt to obtain a competitive position and also to ll a technology vacuum that continued to grow. The section that follows summarizes the key functional features of analog electronic controls in

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