The kinematic structure was designed for a new type of pitch-decoupled vertical take-off and landing UAV (VTOL UAV), based on which the equations and matrix describing its kinematics were derived. The kinematics equations were derived based on Denavit-Hartenberg’s method for robot manipulators, considering the VTOL UAV as a robotic system and its connections as kinematic connection links of the robot. A reference frame was assigned to each of the separate links, from which the transition to the coordinate system of the next link was described by a homogeneous transformation matrix. For each link, its position with respect to its own reference frame was calculated. Based on that, the kinematics matrix was derived, which allows for calculating the required torques of the UAV. In the MATLAB SIMULINK environment, an UAV control system was designed that is based on the kinematic matrix and linear, rotational motion dynamics equations. To check the system’s operability, a proportional, Integral-Derivative (PID) regulator with pre-selected coefficients was selected as a regulator. System research was carried out with pitch, roll, yaw, and decoupled pitch axes as well as height axis.
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