The invention discloses a
finite time control method for a quadrotor aircraft based on an exponentially enhanced exponential approach law and a fast
terminal sliding mode surface. The method comprisesthe following steps: 1, determining a
transfer matrix from a body coordinate
system based on the quadrotor aircraft to an
inertial coordinate system based on the earth; 2, analyzing a quadrotor aircraft
kinetic model according to the Newton-Euler equation; 3, calculating a
tracking error, and designing a controller according to the fast
terminal sliding mode surface and a first-order derivative thereof. Aiming at a quadrotor aircraft
system, the method combines the exponentially enhanced exponential approach law control and the fast
terminal sliding mode control, so the method can increase the approach speed during departing from the sliding mode surface, also can reduce the
jitter, improves the quickness and robustness of the
system, achieves the quick and stable control, also can achieve the
finite time control of the
tracking error, and solves a problem that only when time approaches to infinity in the conventional sliding mode surface, can the
tracking error approach to zero.