Haibo Zhang

Orcid: 0000-0001-9165-9211

Affiliations:
  • Nanjing University of Aeronautics and Astronautics, Nanjing, China


According to our database1, Haibo Zhang authored at least 19 papers between 2011 and 2023.

Collaborative distances:
  • Dijkstra number2 of five.
  • Erdős number3 of four.

Timeline

Legend:

Book 
In proceedings 
Article 
PhD thesis 
Dataset
Other 

Links

Online presence:

On csauthors.net:

Bibliography

2023
An adaptive matching control method of multiple turboshaft engines.
Eng. Appl. Artif. Intell., 2023

Research of Comprehensive Modeling of Two-Dimensional Vector Nozzle/Actuator Load/Turbofan Engine.
IEEE Access, 2023

2022
Design and test of adaptive torsional vibration suppression method for helicopter power system with variable rotor speed.
J. Syst. Control. Eng., 2022

Research and verification on aero-propulsion system acceleration control under supersonic state.
J. Syst. Control. Eng., 2022

2021
Aero-engine dynamic model based on an improved compact propulsion system dynamic model.
J. Syst. Control. Eng., 2021

2020
Aero-engine direct thrust control with nonlinear model predictive control based on linearized deep neural network predictor.
J. Syst. Control. Eng., 2020

Research on aero-engine steady model based on an improved compact propulsion system model.
J. Syst. Control. Eng., 2020

A study on global optimization and deep neural network modeling method in performance-seeking control.
J. Syst. Control. Eng., 2020

2019
A Study of Aero-Engine Control Method Based on Deep Reinforcement Learning.
IEEE Access, 2019

Aero-Engine On-Board Model Based on Batch Normalize Deep Neural Network.
IEEE Access, 2019

A Study on the Acceleration Optimization Control Method for the Integrated Helicopter/Engine System Based on Torsional Vibration Suppression.
IEEE Access, 2019

LPV/PI Control for Nonlinear Aeroengine System Based on Guardian Maps Theory.
IEEE Access, 2019

The Installation Performance Control of Three Ducts Separate Exhaust Variable Cycle Engine.
IEEE Access, 2019

2018
Aero-Engine On-Board Dynamic Adaptive MGD Neural Network Model Within a Large Flight Envelope.
IEEE Access, 2018

Adaptive Control and Predictive Control for Torsional Vibration Suppression in Helicopter/Engine System.
IEEE Access, 2018

2017
On-board real-time optimization control for turbofan engine thrust under flight emergency condition.
J. Syst. Control. Eng., 2017

2012
An improved recursive reduced least squares support vector regression.
Neurocomputing, 2012

2011
Pruning least objective contribution in KMSE.
Neurocomputing, 2011

A fast method of feature extraction for kernel MSE.
Neurocomputing, 2011


  Loading...