Lianghua Sun

Fast terminal sliding mode control based on extended state observer for swing nozzle of anti-aircraft missile

Ran Yi, Weihong Wang, Wulong Zhang, 2015 .

A novel guidance law using fast terminal sliding mode control with impact angle constraints.

Weihong Wang, Ran Yi, Lianghua Sun, 2016, ISA transactions.

Nonlinear attitude control using extended state observer for tilt-rotor aircraft

Ke Lu, Weihong Wang, Siyang Song, 2015, The 27th Chinese Control and Decision Conference (2015 CCDC).

Strictly-lower-convex-function-constructing disturbance observer based adaptive back stepping control for hypersonic flight vehicles

Yun-jie Wu, Lianghua Sun, Jing-xing Zuo, 2018 .

Smooth backstepping sliding mode control for missile attitude system based on parameters online adjusting and estimating for square of disturbance upper bound

Yun-jie Wu, Lianghua Sun, Jing-xing Zuo, 2019 .