Flight Stability Analysis of a Symmetrically-Structured Quadcopter Based on Thrust Data Logger Information

Quadcopter flight stability is achieved when all of the rotors–propellers generate equal thrust in hover and throttle mode. It requires a control system algorithm for rotor speed adjustment, which is related with the translational vector and rotational angle. Even with an identical propell...

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Bibliographic Details
Main Authors: Endrowednes Kuantama, Ioan Tarca, Simona Dzitac, Ioan Dzitac, Radu Tarca
Format: Article
Language:English
Published: MDPI AG 2018-07-01
Series:Symmetry
Subjects:
Online Access:http://www.mdpi.com/2073-8994/10/7/291