The invention discloses a quad-rotor guaranteed performance quantitative control method considering airborne resource limitation, and relates to the technical field of quad-rotor
automatic control. The method comprises the following steps: firstly, establishing a motion /
kinetic model which considers control input quantification and can represent
strong coupling and strong uncertainty of the quadrotor; secondly, designing a mixed event triggering function based on a fixed threshold value and a relative threshold value, and constructing a mixed event triggering extended
state observer for a track and an attitude loop respectively; then, establishing a four-rotor trajectory
tracking error conversion model by utilizing a preset
performance control principle to ensure that the trajectory tracking performance meets preset transient and steady
performance index requirements; further, designing a quad-rotor trajectory loop
virtual control law, and generating quad-rotor
centroid dynamics
virtual control input and an expected course angle instruction through
inverse dynamics calculation; and finally, designing a quad-rotor virtual
attitude control law. The quadrotor trajectory
loop control precision is greatly improved, and finally effective utilization of airborne resources under a guaranteed performance framework is achieved.