Backstepping Control Method of Quadrotor UAV with Input Time Delay
A four-rotor unmanned aerial vehicle, backstep control technology, applied in the direction of attitude control, control/adjustment system, non-electric variable control, etc., can solve the problems of control signal control, accidents, system divergence, etc., to reduce the arrival time, avoid Excessive overshoot, the effect of improving control accuracy
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[0069] The technical solutions of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention.
[0070] refer to Figure 1-Figure 3 , a method for backstepping control of a quadrotor UAV with an input time delay, comprising the following steps:
[0071] Step 1, establish the dynamic model of the four-rotor UAV system, set the initial value, sampling time and relevant control parameters of the system, the process is as follows:
[0072] To model the flight dynamics of the quadrotor UAV, the linear form of the dynamics model is:
[0073]
[0074] in is the roll angle; θ is the pitch angle; ψ is the yaw angle; m is the total mass of the drone body; U 1 is the input of the vertical channel; τ is the unknown input delay; l is the distance from the center of the propeller to the center of the quadrotor; I x , I y , I z are the moment of inertia of the quadrotor to the three axe...
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