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From the Test Benches to the First Prototype of the muFly Micro Helicopter
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From the Test Benches to the First Prototype of the muFly Micro Helicopter
Dario Schafroth1 , Samir Bouabdallah1 , Christian Bermes1 and Roland Siegwart1 
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Autonomous System Lab, Swiss Federal Institute of Technology Zurich (ETHZ), Zurich, Switzerland |
Received: 15 March 2008 Accepted: 30 June 2008 Published online: 23 July 2008
Abstract The goal of the European project muFly is to build a fully autonomous micro helicopter, which is comparable to a small bird
in size and mass. The rigorous size and mass constraints infer various problems related to energy efficiency, flight stability
and overall system design. In this research, aerodynamics and flight dynamics are investigated experimentally to gather information
for the design of the helicopter’s propulsion group and steering system. Several test benches are designed and built for these
investigations. A coaxial rotor test bench is used to measure the thrust and drag torque of different rotor blade designs.
The effects of cyclic pitching of the swash plate and the passive stabilizer bar are studied on a test bench measuring rotor
forces and moments with a 6–axis force sensor. The gathered knowledge is used to design a first prototype of the muFly helicopter.
The prototype is described in terms of rotor configuration, structure, actuator and sensor selection according to the project
demands, and a first version of the helicopter is shown. As a safety measure for the flight tests and to analyze the helicopter
dynamics, a 6DoF vehicle test bench for tethered helicopter flight is used.
Keywords MAV - Test bench - Coaxial - Aerodynamics - Stability - Design - Flight test
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