TY - GEN
T1 - Approximation of thrust generated by rotor in quadrotor unit with use of generalized polynomial
AU - Binias, Bartosz
AU - Grzejszczak, Tomasz
AU - Janusz, Wojciech
AU - Niezabitowski, Michal
N1 - Publisher Copyright:
© 2016 IEEE.
PY - 2016/8/5
Y1 - 2016/8/5
N2 - This paper presents the way of modeling thrust generated by a quadrotor flying unit. The highly non-linear equations describing rotor thrust are derived with use of momentum theory and approximated with use of generalized polynomial. The article includes the model formulation and the example of approximation. The polynomial approximation ensures the simplicity in solving during simulation with sufficient accuracy.
AB - This paper presents the way of modeling thrust generated by a quadrotor flying unit. The highly non-linear equations describing rotor thrust are derived with use of momentum theory and approximated with use of generalized polynomial. The article includes the model formulation and the example of approximation. The polynomial approximation ensures the simplicity in solving during simulation with sufficient accuracy.
UR - https://www.scopus.com/pages/publications/84986237937
U2 - 10.1109/MED.2016.7535949
DO - 10.1109/MED.2016.7535949
M3 - Conference contribution
AN - SCOPUS:84986237937
T3 - 24th Mediterranean Conference on Control and Automation, MED 2016
SP - 415
EP - 419
BT - 24th Mediterranean Conference on Control and Automation, MED 2016
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 24th Mediterranean Conference on Control and Automation, MED 2016
Y2 - 21 June 2016 through 24 June 2016
ER -