Two controller designs of hypersonic flight vehicle under actuator dynamics and AOA constraint

Y Guo, B Xu, X Hu, X Bu, Y Zhang - Aerospace Science and Technology, 2018 - Elsevier
This paper studies the controller design for hypersonic flight vehicle (HFV) considering the
actuator hysteresis and the angle of attack (AOA) constraint respectively. Firstly, the effect of …

[HTML][HTML] Fixed-time adaptive model reference sliding mode control for an air-to-ground missile

L Zhang, WEI Changzhu, WU Rong… - Chinese Journal of …, 2019 - Elsevier
This paper addresses the fixed-time adaptive model reference sliding mode control for an air-
to-ground missile associated with large speed ranges, mismatched disturbances and un …

A robust adaptive control approach to missile autopilot design

AN Ouda - International Journal of Dynamics and Control, 2018 - Springer
The huge developments in computational capabilities facilitate the design and
implementation of adaptive and robust control. Furthermore, the great developments in …

Self-evolving data cloud-based PID-like controller for nonlinear uncertain systems

ZX Yang, HJ Rong, PK Wong, P Angelov… - IEEE Transactions …, 2020 - ieeexplore.ieee.org
In this article, a novel self-evolving data cloud-based proportional integral derivative
(PID)(SEDCPID) like controller is proposed for uncertain nonlinear systems. The proposed …

A deep learning based method for blind recognition of LDPC codes

L Li, L Xie, Z Huang, C Liu, J Zhou… - 2021 2nd Information …, 2021 - ieeexplore.ieee.org
Deep learning is an emerging research direction in machine learning, which has a
promising application in the field of communications. In this paper, we focus on adaptive …

Adaptive nonparametric evolving fuzzy controller for uncertain nonlinear systems with dead zone

ZX Yang, ZX Yang, HJ Rong - Evolving Systems, 2022 - Springer
This paper presents an adaptive nonparametric evolving fuzzy controller for uncertain
nonlinear systems with dead zone. The unknown nonlinear-ities caused by the dead zone …

Precise Missile Autopilot Design Using Nonlinear Sliding Mode Control

J Liao, H Bang - 2022 13th Asian Control Conference (ASCC), 2022 - ieeexplore.ieee.org
This paper presents a nonlinear sliding mode control (SMC) based autopilot system design
for precise missile operation, saturation function is introduced to avoid chattering problem …

Performance Analysis of a Twin Rotor MIMO System Using Fuzzy Logic Controller

P Das, PR Bhutia, RK Mehta, OP Roy - International Conference on …, 2019 - Springer
This study explains about the MIMO plant statistics of fuzzy logic based control of a electro-
mechanical system. An intelligent control system is proposed here in this paper to observe …

Adaptive Self-Learning Fuzzy Autopilot Design for Uncertain Bank-To-Turn Missiles

HJ Rong, ZX Yang - Sequential Intelligent Dynamic System Modeling and …, 2024 - Springer
This chapter presents an adaptive self-learning fuzzy autopilot design for uncertain bank-to-
turn missiles due to external disturbances and system errors from the variations of the …