DocumentCode :
3491435
Title :
Aerodynamics and flight control design for hovering micro air vehicles
Author :
Motazed, Ben ; Vos, David ; Drela, Mark
Author_Institution :
Aurora, Manassas, VA, USA
Volume :
2
fYear :
1998
fDate :
21-26 Jun 1998
Firstpage :
681
Abstract :
A general overview is presented on a new area of development, namely the 15-cm and smaller micro air vehicle (MAV) technology. The general set of postulated mission requirements is the driver for the design configuration and performance specifications for this class of aircraft. Low Reynolds number and thus low aerodynamic efficiency, power density, weight, and stability in the presence of gust are significant technical challenges for the MAV-sized class of platforms to conduct long-endurance and range missions. A 15-cm hovering MAV concept is presented, with design attributes to circumvent the stabilization and control issues associated with the conventional helicopter. Aerodynamic, stabilization, and control approaches and analysis are presented
Keywords :
aerodynamics; aircraft control; control system synthesis; mobile robots; stability; 0 to 15 cm; MAV; aerodynamic efficiency; aerodynamics; flight control design; gust; hovering micro air vehicles; power density; stability; weight; Aerodynamics; Aerospace control; Blades; Inspection; Landmine detection; Military computing; Propulsion; Rotors; Space technology; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1998. Proceedings of the 1998
Conference_Location :
Philadelphia, PA
ISSN :
0743-1619
Print_ISBN :
0-7803-4530-4
Type :
conf
DOI :
10.1109/ACC.1998.703492
Filename :
703492
Link To Document :
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