Navigation Functionalities for an Autonomous UAV Helicopter
Navigation Functionalities for an Autonomous UAV Helicopter
Navigation Functionalities for an Autonomous UAV Helicopter
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Chapter 4<br />
Path Following Control<br />
Mode<br />
4.1 Introduction<br />
The PFCM described in this chapter <strong>an</strong>d presented in Paper I, has been<br />
designed to navigate <strong>an</strong> autonomous helicopter in <strong>an</strong> area cluttered with<br />
obstacles, such as <strong>an</strong> urb<strong>an</strong> environment. In this thesis, the path pl<strong>an</strong>ning<br />
problem is not addressed although it is in [18]. It is assumed that a<br />
path pl<strong>an</strong>ning functionality generates a collision-free path. Then the task<br />
which will be solved here is to find a suitable guid<strong>an</strong>ce <strong>an</strong>d control law<br />
which enables the helicopter to follow the path robustly. The path pl<strong>an</strong>ner<br />
calculates the geometry of the path that the helicopter has to follow. A<br />
geometric path segment, represented by a set of parameters, is then input<br />
to the PFCM.<br />
Be<strong>for</strong>e starting with the description of the PFCM, some basic terminology<br />
will be provided.<br />
The guid<strong>an</strong>ce is the process of directing the movements of <strong>an</strong> aeronautical<br />
vehicle with particular reference to the selection of a flight path.<br />
The term of guid<strong>an</strong>ce or trajectory generation in this thesis addresses the<br />
problem of generating the desired reference position <strong>an</strong>d velocity <strong>for</strong> the<br />
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