DocumentCode :
1875972
Title :
Platform description and system modelling for control of an unmanned helicopter
Author :
Koslowski, Markus ; Kandil, Amr A. ; Badreddin, Essameddin
Author_Institution :
Autom. Lab., Univ. of Heidelberg, Mannheim, Germany
fYear :
2012
fDate :
6-8 Sept. 2012
Firstpage :
391
Lastpage :
396
Abstract :
This paper presents the Scout B1-100 autonomous unmanned helicopter platform and an appropriate mathematical model for the hovering flight. The assembly of the experimental helicopter platform and its different hardware components are depicted. A dynamical model of the helicopter is derived from first principles and then linearized to obtain system description in state space. The model can be used for controller design in hovering flight. The model parameters are determined using time domain identification techniques. The identified model has been also validated.
Keywords :
aircraft control; autonomous aerial vehicles; control system synthesis; helicopters; state-space methods; time-domain analysis; Scout B1-100 autonomous unmanned helicopter platform; controller design; dynamical model; experimental helicopter platform assembly; hardware components; hovering flight; mathematical model; model parameters; platform description; state space; system description; system modelling; time domain identification techniques; unmanned helicopter control; Aerodynamics; Computational modeling; Equations; Helicopters; Mathematical model; Rotors; UAV; autonomous helicopter; mathematical modeling; system identification;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Systems (IS), 2012 6th IEEE International Conference
Conference_Location :
Sofia
Print_ISBN :
978-1-4673-2276-8
Type :
conf
DOI :
10.1109/IS.2012.6335248
Filename :
6335248
Link To Document :
بازگشت