E3S Web Conf.
Volume 233, 20212020 2nd International Academic Exchange Conference on Science and Technology Innovation (IAECST 2020)
|Number of page(s)||10|
|Section||MEA2020-Mechanical Engineering and Automation|
|Published online||27 January 2021|
Fault tolerant control of uav with wing layout based on control allocation
1 Combat college, naval aviation university, yantai, 264001, Shandong, China
2 Army 92692 Fujian Zhanjiang 524000.)
As the flying wing layout unmanned aerial vehicle (uav) extensive research and task environment increasingly complex, Yu Feiyi layout unmanned aerial vehicle (uav) for fault tolerant control gradually become the main technical means of the flight control, using the established mathematical model of the flying wing uav longitudinal layout setting the actuator failure effect, is in the nature of adaptive control allocation fault-tolerant algorithm is given, and MATLAB/simulink simulation is carried out for uav longitudinal motion, realize the rapid and stable, the control command and response to complete the nonlinear fault-tolerant control of flying wing uavs.
© The Authors, published by EDP Sciences 2021
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