Open AccessFlight optimisation of missile using linear matrix inequality (LMI) approach
Author(s) -
Deb Majumder Samarpan
Publication year - 2020
Publication title -
the journal of engineering
Language(s) - English
Resource type - Journals
ISSN - 2051-3305
DOI - 10.1049/joe.2019.0952
Subject(s) - autopilot , missile , aerodynamics , angle of attack , finite element method , control theory (sociology) , linear matrix inequality , matrix (chemical analysis) , computer science , mathematics , aerospace engineering , engineering , mathematical optimization , control (management) , structural engineering , artificial intelligence , materials science , composite material
The research entails a finite‐element design of a 3d‐autopilot missile synthesis of multiple objective controls by solving the inequalities encountered while using a linear matrix. The autopilot design analyses the performance methodologies for a group of finite models that are further linearised at different aerodynamic roll angles within the flight coverage for harnessing the uncertainties that are encountered confined within the high angle‐of‐attack region. Multiple simulation results are devised at various roll angle conditions to satisfy the performance of the controls.