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Section  3.8  Design  Examples                                      193

       3.8  DESIGN  EXAMPLES

                        In this section we present two illustrative design examples. In the first example, we pre-
                       sent a detailed  look at modeling a large space vehicle (such as a space station)  using a
                       state variable model. The state variable model is then used to take a look at the stability
                        of the orientation  of the spacecraft  in a low earth orbit. The design process depicted in
                       Figure  1.15  is highlighted  in  this  example. The second  example  is a printer  belt  drive
                       modeling exercise. The relationship between the state variable model and the block dia-
                       gram discussed in Chapter 2 is illustrated and, using block diagram reduction methods,
                       the transfer function  equivalent  of the state variable model is obtained.

                       EXAMPLE 3.7    Modeling the orientation  of a space station
                       The International  Space Station, shown in Figure  3.27, is a good  example  of a multi-
                       purpose  spacecraft  that  can  operate  in many  different  configurations. An  important
                       step in the  control  system  design process  is to develop a mathematical  model  of  the
                       spacecraft motion. In general, this model describes the translation and attitude motion
                       of the spacecraft  under the influence  of external forces and torques, and controller and
                       actuator  forces  and torques. The resulting spacecraft  dynamic model is a set  of highly
                       coupled,  nonlinear  ordinary  differential  equations.  Our  objective  is  to  simplify  the
                       model while retaining important system characteristics. This is not a trivial task, but an
                       important, and often neglected component  of control engineering. In this example, the
                       rotational motion is considered. The translational motion, while critically important to
                       orbit maintenance, can be decoupled from the rotational motion.
                           Many  spacecraft  (such  as  the  International  Space  Station)  will  maintain  an
                       earth-pointing  attitude. This  means  that  cameras  and  other  scientific  instruments
                       pointing down will be able to sense the earth, as depicted in Figure 3.27. Conversely,






















       FIGURE  3.27
      The International
      Space Station
      moments after the
      Space Shuttle
      undocked from the
      Station.  (Courtesy
      of  NASA.)
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