Implementation of speed and torque control on quadrotor altitude and attitude stability
Most quadrotor flight controllers make use of an attitude control loop, which is responsible for stabilizing the flight of the vehicle by directly driving the four motors via the electronic speed controllers (ESCs). Such a control loop loses its effectiveness when the motors and ESCs are not well ma...
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Main Authors: | , , , , , |
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Format: | text |
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Animo Repository
2013
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Online Access: | https://animorepository.dlsu.edu.ph/faculty_research/7917 |
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Institution: | De La Salle University |
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