Comprehensive Review of Metaheuristic Algorithms (MAs) for Optimal Control (OCl) Improvement

U Mohammed, T Karataev, O Oshiga… - … Methods in Engineering, 2024 - Springer
Optimal control (OCl) can be traced back to the 1960s when it was utilised for solving an
optimisation problem (OP). In the OCl technique, a stable controller can be obtained by …

Linear quadratic Gaussian control for wireless communication reliability for a mobile monitoring robot in a UHV power substation

W Sun, K Wei, Z Liu, Q Li, X Xu - IEEE Systems Journal, 2022 - ieeexplore.ieee.org
In ultrahigh-voltage (UHV) power substations, mobile robots equipped with sensors and
cameras have been adopted for patrolling and inspecting the operational status of devices …

[PDF][PDF] Pitch control of a rocket with a novel LQG/LTR control algorithm

AB Kisabo, AF Adebimpe, SO Samuel - J. Aircr. Spacecr. Technol, 2019 - researchgate.net
This paper presents the design, simulation and analysis of a novel LQG and LQG/LTR
control algorithm for the pitch angle of a sounding rocket. These improved LQG and …

Transformation of LQR weights for discretization invariant performance of PI/PID dominant pole placement controllers

K Halder, S Das, A Gupta - Robotica, 2020 - cambridge.org
Linear quadratic regulator (LQR), a popular technique for designing optimal state feedback
controller, is used to derive a mapping between continuous and discrete time inverse …

Aircraft pitch control design using LQG controller based on genetic algorithm

AI Abdulla, IK Mohammed - … Computing Electronics and …, 2023 - telkomnika.uad.ac.id
Designing a robust aircraft control system used to achieve a good tracking performance and
stable dynamic behavior against working disturbances problem has attracted attention of …

Optimal trajectory generation and tracking for a helicopter in tail rotor failure

YO Arslan - 2022 - open.metu.edu.tr
Tail rotor failure is the main reason for a variety of helicopter accidents throughout aviation
history. It is troublesome to control and navigate the helicopter to a predefined landing point …

Investigative design of missile longitudinal dynamics using LQR-LQG controller in presence of measurement noise and inaccurate model

VSNM Arikapalli, S Bhowmick, PB Rao, R Ayyagari - Sādhanā, 2022 - Springer
The paper presents the design and development of a Linear Quadratic Gaussian (LQG)
controller for a longitudinal dynamics of a high maneuvering missile. The Linear Quadratic …

Model-Free Perception-Based Control via Q-Learning with an Application to Heat-Seeking Missile Guidance

WS Kovalik, L Zhai… - 2021 IEEE Conference on …, 2021 - ieeexplore.ieee.org
Modern perception-based sensing schemes incorporate machine learning and high-
dimensional image observations to control system states, but face issues of perception error …

A novel SHLNN based robust control and tracking method for hypersonic vehicle under parameter uncertainty

C Li, H Wu, Z Yang, Y Wang, Z Sun - Complexity, 2017 - Wiley Online Library
Hypersonic vehicle is a typical parameter uncertain system with significant characteristics of
strong coupling, nonlinearity, and external disturbance. In this paper, a combined system …

A Self-tuning controller design method based on LQG/LTR and back propagation algorithm

W Liu, Z Hu, J Wang, S Liu - Proceedings of 2019 Chinese Intelligent …, 2020 - Springer
A self-tuning controller design method, based on the Back Propagation (BP) algorithm, was
proposed to tune the LQG/LTR gain matrices directly without the need of selecting weighting …