This chapter discusses some basic concepts related to the large angle non‐linear flight mechanics equations of motion of the aircraft, when undergoing dynamic manoeuvres. It focuses on ideas relevant to the response and hence internal loads in dynamic manoeuvres. An approach based on scalars is used in order to provide a little more physical appreciation and to avoid an excursion into vectors for only a limited part of the book; however, it must be emphasized that a vector approach is simpler and more elegant for the 3D case. Later in the chapter, the linearized flight mechanics model is applied to the problems of a rigid or flexible aircraft undergoing a dynamic manoeuvre in heave/pitch; these symmetric cases allow some basic concepts to be seen using a small order mathematical model. The response, dynamic stability modes and control effectiveness are calculated.
Dynamic Manoeuvres
02.12.2014
45 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Wiley | 2014
|Wiley | 2021
|Wiley | 2014
|British Library Online Contents | 1996
Wiley | 2021
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