Supersonic Missile Control with PI Sliding Mode Method
Comparing with traditional adaptive methods, a very simple PI sliding mode controller is designed for uncertain nonlinear missile systems with the help of two main assumptions which are also testified to be reasonable.The construction of PI control for sliding surface is novel and effective. Also, the proof of PI type control law is unique in this paper.
Pengcheng Wang, Liqun Ai, Yungang Li, Xiaoming Sang and Jinglong Bu
Q. Ma and Y. Q. Jin, "Supersonic Missile Control with PI Sliding Mode Method", Advanced Materials Research, Vols. 295-297, pp. 1773-1776, 2011