The Advanced Aircraft Analysis (AAA) software provides a powerful framework to support the iterative and nonunique process of aircraft preliminary design. The AAA program allows design engineers to rapidly evolve a preliminary aircraft configuration from early weight sizing through open-loop and closed-loop dynamic stability and sensitivity analysis, while working within civil and military regulations and cost constraints.
The design methodology used in the development of the AAA program is based on Airplane Design, Parts I through VIII, and Airplane Flight Dynamics, Parts I and II, by Dr. Jan Roskam.
William A. Anemaat
Chief Engineer Design, Analysis and Research Corporation 120 East Ninth Street Suite 2 Lawrence, KS 66044 USA 913-832-0434 fax:913-832-0524