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Please use this identifier to cite or link to this item: http://hdl.handle.net/1853/29661

Title: Design, testing, and performance of a hybrid micro vehicle - the hopping rotochute
Authors: Beyer, Eric W.
Aerospace Engineering
Advisor: Committee Chair: Costello, Mark
Subjects : Hopping
Micro air vehicle
Rotorcraft
Aerodynamics
Lifting bodies (Aeronautics) Flight testing
DYNAMO (Computer program language)
Mobile robots
Robots
Issue Date: 4-May-2009
Publisher: Georgia Institute of Technology
Abstract: A new hybrid micro vehicle, called the Hopping Rotochute, was developed to robustly explore environments with rough terrain while minimizing energy consumption over extended periods of time. Unlike traditional robots, the Hopping Rotochute maneuvers through complex terrain by hopping over or through impeding obstacles. A small coaxial rotor system provides the necessary lift while a movable internal mass controls the direction of travel. In addition, the low mass center and egg-like shaped body creates a means to passively reorient the vehicle to an upright attitude when in ground contact while protecting the rotating components. The design, fabrication, and testing of a radio-controlled Hopping Rotochute prototype as well as an analytical study of the flight performance are documented. The aerodynamic, mechanical, and electrical design of the prototype is outlined which were driven by the operational requirements assigned to the vehicle. The aerodynamic characteristics of the rotor system as well as the damping characteristics of the foam base are given based on experimental results using a rotor test stand and a drop test stand respectively. Experimental flight testing results using the prototype are outlined which demonstrate that all design and operational requirements are satisfied. A dynamic model associated with the Hopping Rotochute is then developed including a soft contact model which estimates the forces and moments on the vehicle during ground contact. A comparison between the vehicle's motion measured using a motion capture system and the simulation results are presented to determine the validity of the experimentally-tuned dynamic model. Using this validated simulation model, key parameters such as system weight, rotor speed profile, internal mass weight and location, as well as battery capacity are varied to explore the flight performance characteristics. The sensitivity of the hopping rotochute to atmospheric winds is also investigated as well as the ability of the device to perform trajectory shaping.
Type: Dissertation
URI: http://hdl.handle.net/1853/29661
Appears in Collections:School of Aerospace Engineering Theses and Dissertations
Georgia Tech Theses and Dissertations

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