[PDF][PDF] A robust control approach for rocket landing

R Ferrante - Theses Univ. Edinburgh, 2017 - project-archive.inf.ed.ac.uk
The high cost of rocket technology has led to system reusability developments, particularly in
the field of first stage rockets. With the motivation of decreasing production costs, successful …

Design of gain schedule fractional PID control for nonlinear thrust vector control missile with uncertainty

M Fawzy Ahmed, H Taher Dorrah - Automatika: časopis za automatiku …, 2018 - hrcak.srce.hr
Sažetak The purpose of this paper is to control the trajectory of the nonlinear missile model
in the pitch channel by using Fractional PID controller (FPID) and Gain Schedule Fractional …

Adaptive control designed by online solving for Riccati and Lyapunov equations with nonlinear flight body

MF Ahmed, HT Dorrah - International Journal of Automation …, 2020 - inderscienceonline.com
The aim of this paper is to control the path for nonlinear missile model in the pitch channel
using model reference adaptive control (MRAC) and L 1 adaptive control with linear …

[HTML][HTML] 基于滚动时域优化的旋转弹解耦控制器设计

陈伟, 孙传杰, 冯高鹏, 拜云山 - 2018 - html.rhhz.net
旋转弹在飞行过程中会受到外界干扰和不确定性的影响, 并且存在气动交联,
惯性交联和控制交联, 为了实现稳定飞行, 有必要进行解耦控制器设计. 提出了一种基于滚动时域 …

Comparison of the Performance of PID and TVLQR Controllers for Nonlinear Modelling of a Freedom Flying Body.

M Fawzy, H Attar, A Amer, S Alsaqoor… - Przeglad …, 2024 - search.ebscohost.com
English The aim of the research was to enhance the trajectory control of a nonlinear freedom
flying body model by comparing time-varying linear quadratic regulator (TVLQR) controller …

Rate Autopilots for Guided Aerial Bomb

M Ignjatović, M Ristanović, A Trifković… - 2024 11th …, 2024 - ieeexplore.ieee.org
This paper shows the possibility of implementing model predictive control algorithm as rate
autopilot for guided aerial bomb. Mathematical model that is used for transfer function …

基于离线预测控制的旋转尾翼稳定弹解耦控制器设计

陈伟, 孙传杰, 李永泽, 拜云山 - 兵工学报, 2018 - co-journal.com
低速旋转尾翼稳定弹飞行过程中存在着气动交联, 惯性交联和控制交联, 为了实现稳定飞行,
有必要进行解耦控制器设计. 鉴于模型预测控制方法虽然具有较好的解耦能力和对建模精度要求 …

[HTML][HTML] Optimization of the Integrated Guidance and Control for a Dual Aerodynamic Control Missile

FBI Hernández - 2015 - dialnet.unirioja.es
Las futuras misiones para misiles aire-aire operando dentro de la atmósfera requieren la
interceptación de blancos a mayores velocidades y más maniobrables, incluyendo los …

Tổng hợp thuật toán điều khiển thông minh cho một lớp thiết bị bay

T Trantuandon, QH Nguyễn, QV Nguyễn… - Journal of Military …, 2024 - ojs.jmst.info
Autonomous aerial vehicles in the Navy are modern aircraft widely used in military
applications. Current techniques are primarily based on linear control theory, which may …

[PDF][PDF] Hata Tolerans Kontrollü ve Model Öngörülü Füze Kontrolcü Tasarımı

Y Önay, SÇ Baslamıslı - researchgate.net
Aerospace defence industry has been a critical field for control design and application. In
order to control swift motions of aircrafts in dynamic environments benefiting from control …