The invention provides an aircraft
attitude control method, a
system, a medium and a device, wherein the method comprises the following steps: establishing a sliding hyperplane and a sliding mode approaching law according to attitude tracking errors, control law parameters and approaching law parameters; establishing an expansion
state observer, and using the expansion
state observer to estimate atotal uncertainty in a
mathematical model of an aircraft; obtaining an
attitude control law according to the sliding hyperplane, the sliding mode approaching law, and the expansion
state observer; and controlling the attitude of the aircraft according to the
attitude control law. The aircraft attitude control method, the
system, the medium and the device can avoid
singular problems caused by thetraditional
terminal sliding mode control method according to an improved
sliding mode control of a fast non-singular terminal, which have a higher convergence rate that can converge errors more quickly in comparison with the traditional non-singular
terminal sliding mode control. In addition, by combining the expansion state observer, discontinuous term gains can be reduced, sliding mode chattering can be weakened, and the robustness of the
system can be improved through interference
estimation and compensation.