| 摘要 |
A stabilization system of a pilotless aircraft on aerial inspection trajectories comprises a setting device, a first adder, a controller, an object of control, an integrator, a second adder, while the output of setting device is connected to a summing input of the first adder, whose output is connected to the input of controller, the controller output is connected to the input of controlled object and the first input of second adder, the output of controlled object is connected to the second input of first adder, the output of second adder is connected to the input of integrator, whose output is connected to the respective input of first adder and the second input of second adder. The system is implemented as a set of an ideal control circuit and an adaptation circuit performing functions of a quasi-adaptive controller, the controller is designed as a square controller. |
