Control analysis with modified LQR method of anti-tank missile with vectorization of the rocket engine thrust

Ł Nocoń, M Grzyb, P Szmidt, Z Koruba, Ł Nowakowski - Energies, 2022 - mdpi.com
This article approaches the issue of the optimal control of a hypothetical anti-tank guided
missile (ATGM) with an innovative rocket engine thrust vectorization system. This is a highly …

Tuning of a linear-quadratic stabilization system for an anti-aircraft missile

W Bużantowicz - Aerospace, 2021 - mdpi.com
A description is given of an application of a linear-quadratic regulator (LQR) for stabilizing
the characteristics of an anti-aircraft missile, and an analytical method of selecting the …

A New Statistical Method for Determining the Clutter Covariance Matrix in Spatial–Temporal Adaptive Processing of a Radar Signal

A Kawalec, A Ślesicka, B Ślesicki - Sensors, 2023 - mdpi.com
In this article, a new statistical method for estimating the clutter covariance matrix in space–
time adaptive radar signal processing (STAP) is presented and studied. The new method …

Robust control for uncertain air-to-air missile systems

J Farrington, X Wang - arXiv preprint arXiv:2411.07593, 2024 - arxiv.org
Air-to-air missiles are used on many modern military combat aircraft for self-defence. It is
imperative for the pilots using the weapons that the missiles hit their target first time. The …

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 …

Design and simulation of a longitudinal autopilot system for flying vehicles based on LQR and Luenberger observer

M Ashraf, E Safwat, MAH Abozied… - … on Aerospace Sciences …, 2023 - asat.journals.ekb.eg
A longitudinal autopilot system for flying vehicles, such as missiles and drones, is crucial for
enhancing stability, reducing the risk of errors, improving efficiency, and providing better …

[PDF][PDF] Control Analysis with Modified LQR Method of Anti-Tank Missile with Vectorization of the Rocket Engine Thrust. Energies 2022, 15, 356

M Grzyb, P Szmidt, Z Koruba, Ł Nowakowski - 2022 - academia.edu
This article approaches the issue of the optimal control of a hypothetical anti-tank guided
missile (ATGM) with an innovative rocket engine thrust vectorization system. This is a highly …

[引用][C] Tuning of a Linear-Quadratic Stabilization System for an Anti-Aircraft Missile. Aerospace 2021, 8, 48

W Buzantowicz - 2021 - s Note: MDPI stays neu-tral with …