Further Investigations on Newton-Raphson Methods in Aircraft Trim

This paper is a follow-up on a prior work on aircraft trim using Newton-Raphson methods for steady and level flight, climb or descent, steady turn, and pull-up or push-over flight conditions. The current study extends this work to steady climbing/descending turn, crosswind landing, steady heading steady sideslip, aileron roll, and barrel roll trim conditions based on classical and Line-Search Newton Raphson methods.