AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021, Virtual, Online, 2 - 06 August 2021
© 2021, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.This paper is to follow up on prior research works on aircraft trim. The prior works studied a comparative study of Newton-Raphson and Line Search Newton-Raphson methods in aircraft trim for various steady-state flight conditions, e.g., steady and level flight, climb or descend flight, steady turn flight, pull-up, and push-over flight conditions. In the current research, the Newton Raphson Based Genetic Algorithm is introduced.