DocumentCode
716387
Title
Passive stability of vehicles without angular momentum including quadrotors and ornithopters
Author
Piccoli, Matthew ; Yim, Mark
Author_Institution
Mech. Eng. & Appl. Mech., Univ. of Pennsylvania, Philadelphia, PA, USA
fYear
2015
fDate
26-30 May 2015
Firstpage
1716
Lastpage
1721
Abstract
The paper presents a model for adding stabilizers to a flying device without rotational momentum (such as quadrotors or ornithopters) that will create passively stable vehicles in hover. This model enables the design of the size and location of these stabilizers that will vary the stability and performance of the vehicle. The model is verified with nine experimental vehicles that span the stability design space. Passive stability allows the removal of costly inertial sensors and increases the robustness of the vehicle. Analysis of the cost and drag that impacts flight performance is also discussed.
Keywords
autonomous aerial vehicles; helicopters; mechanical stability; microrobots; angular momentum; flight performance; micro air vehicles; ornithopters; quadrotors; rotational momentum; stability design space; vehicle passive stability; vehicle performance; Aerodynamics; Damping; Eigenvalues and eigenfunctions; Helicopters; Propellers; Stability analysis; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Robotics and Automation (ICRA), 2015 IEEE International Conference on
Conference_Location
Seattle, WA
Type
conf
DOI
10.1109/ICRA.2015.7139419
Filename
7139419
Link To Document