This paper is focused on the dynamic modelling of an unconventional remotely-piloted Lighter-Than-Air vehicle, whose mathematical model is based on a 6 degree-of-freedom, 12 states nonlinear system, described by the basic equations of the Newtonian mechanics. Emphasis is placed on those innovative and peculiar aspects of the dynamic modelling, which allow the development of a complete low-cost-high-fidelity Flight Simulator used both for technical and commercial purposes. In particular, the availability of this tool, featuring real time simulations, is essential for the design, test and implementation of the most suitable flight control system, as well as for the pilot training of this innovative airship.
Mathematical Model for simulation Analysis of a Remotely-Piloted Lighter-than-Air Platform / BATTIPEDE M.; GILI P.; LANDO M.. - In: INTERNATIONAL JOURNAL OF MECHANICS AND CONTROL. - ISSN 1590-8844. - 7:1(2006), pp. 3-14.
|Titolo:||Mathematical Model for simulation Analysis of a Remotely-Piloted Lighter-than-Air Platform|
|Data di pubblicazione:||2006|
|Appare nelle tipologie:||1.1 Articolo in rivista|