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Description
A quadrotor is an unmanned aerial vehicle lifted and propelled by four rotors. The rotor mechanics
and the cross configuration of the four rotors benefit the steering of a quadrotor, and make
quadrotors attractive in research and applications.
The objective of this projeck is to design a control law for the quadrotor system, and implement it in
a hardware in loop real time simulation testbed. With simulation, it is possible to know details of the quadrotor
system and the used control law, such as to decrease the accident occurrence in the real flight.
Organisation
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this project is a group work of 2 to 4 members.
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this project should be done in one week (about 40 hours) after the lecture period of the winter semester 2011.
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a report and a presentation are required before March 24th, 2012.
Document
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