- Volume 14 Issue 2
A general purpose aircraft mission performance analysis program has been developed. The program can be used in design mode or in analysis mode. Fuel weight for a given mission profile can be estimated when the design mode is chosen, while mission time or mission range for a given fuel can be estimated when the analysis mode is chosen. The mission analysis program is written with JAVA and includes GUI(Graphic User Interface) for users' conveniences. With a proper combination of databases for propulsion, aerodynamics and weight, the program can be configured to compute the performance of any type of aircraft. The program is validated by comparing its results with the results of a well known performance analysis program by ADD(Agency for Defense Development).
Aircraft;Mission Profile;Mission Performance
- Hague, D. S., and Rozendaal, H. L., "NSEG-a Segmented Mission Analysis Program for Low and High Speed Aircraft, Vol. I Theoretical Development", NASA CR-2807, 1977.
- URL : http://www.darcorp.com/, accessed [March, 10, 2013].
- URL : http://www.aircraftdesign.com/, accessed [March, 10, 2013].
- Mavris, D. N., Soban, D. S., and Largent, M. C., "An Application of a Technology Impact Forecasting(TIF) Method to an Uninhabited Combat Aerial Vehicle", 1999 AIAA/SAE World Aviation Congress, San Francisco, CA, Oct. 19-21, 1999, SAE/AIAA 1999-01-5633.
- URL : http://en.wikipedia.org/wiki/Java_(programming_language), accessed [March, 10, 2013].
- Bertsekas, P. D., Nonlinear Programming, 2nd ed., Athena Scientific, 1999.
- Chong , E.K.P. , Zak, S.H., An introduction to optimization, Wiley, 2001.
- Bae, S., "A Computer Program for Flight Performance Estimation and Mission Analysis", ASDC-401-950029, Agency for Defense Development, 1995.