Ajoy Kanti Ghosh

Orcid: 0000-0003-1249-9147

According to our database1, Ajoy Kanti Ghosh authored at least 12 papers between 2018 and 2023.

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

Timeline

Legend:

Book 
In proceedings 
Article 
PhD thesis 
Dataset
Other 

Links

On csauthors.net:

Bibliography

2023
Dynamic Surface Neuro-Backstepping Based Flight Control With Asymmetric Output Constraints.
IEEE Trans. Aerosp. Electron. Syst., August, 2023

2022
An Approach Towards the Design of Interval Type-3 T-S Fuzzy System.
IEEE Trans. Fuzzy Syst., 2022

Sliding-Mode Control and Strategic Thrust-Vectoring Based Aircraft Flat Spin Recovery With Altitude Loss Minimization.
IEEE Trans. Aerosp. Electron. Syst., 2022

An application of interval type-2 fuzzy model based control system for generic aircraft.
Appl. Soft Comput., 2022

Longitudinal Aerodynamic Parameters Estimation using Machine Learning with Neuro Artificial Bee Colony Fusion Algorithm (NABC).
Proceedings of the 13th Asian Control Conference, 2022

2021
Intelligent Fault Diagnosis of Rotary Machines: Conditional Auxiliary Classifier GAN Coupled With Meta Learning Using Limited Data.
IEEE Trans. Instrum. Meas., 2021

Optimal Energy Utilization for a Solar-Powered Aircraft Using Sliding-Mode-Based Attitude Control.
IEEE Trans. Aerosp. Electron. Syst., 2021

Cascaded and Non-Cascaded Incremental Nonlinear Dynamic Inversion Flight Control Applied to a Light Aircraft.
Proceedings of the 2021 Australian & New Zealand Control Conference, 2021

2020
Simulation and Analysis of Spring Based Transverse Axis Sensing MEMS Capacitive Accelerometer.
Proceedings of the 7th International Conference on Control, 2020

Real-time vision-based tracking of a moving terrain target from Light Weight Fixed Wing UAV using gimbal control.
Proceedings of the 7th International Conference on Control, 2020

2018
Interval type-2 TS fuzzy model for angle of attack sensor of the aircraft.
J. Intell. Fuzzy Syst., 2018

Time-Varying Non-Singular Terminal Sliding Mode Attitude Control of Reusable Launch Vehicle.
Proceedings of the 15th International Conference on Control, 2018


  Loading...