Finite-time Formation Control of Fixed-Wing Aircraft under Constrained Velocity and Acceleration
Disha Zhu, Jianying Yang · 2021
In this paper, based on sliding mode technique, a finite-time formation control method under constrained velocity and acceleration for fixed-wing aircraft is proposed, which is applied to formation and switching of formation, and the formation of maneuver trajectory is realized. Its finite time convergence under constrained velocity and acceleration is proved, and the simulation results show that the method is effective.