SIMULATION OF FLIGHT THROUGH GUST
Main Article Content
Abstract
A flight simulation programme has been developed on a personal computer using Microsoft
FORTRAN to simulate flight trajectories of a light aircraft by using Six-Degree-of-Freedom
equation of motion. The simulation has been made realistic through pre-programmed the input to
the control surfaces, atmospheric gust during the flight mode. The programme plays an important
role in the evaluation and validation of the aircraft design process. A light aircraft (Cessna 182T)
has been tested through free flight, gliding flight, flight with gust. The results show good trend and
show that the programme could be dependent as a realistic flight test programme.
Article Details
Section
How to Cite
References
- Roskam J., “Flight Dynamics of Rigid and Elastic Airplanes”, Published by Roskam aviation and engineering corporation, Kansas, 66044, 1972.
- McRuer D., Ashkenas I., Graham D., “Aircraft Dynamics and Automatic Control”, Princeton University Press, New
Jersey, 1973.
- Khare Alok, Madhuranath Padma, “SOFT–Simulation of Flight Trajectories”, NAL-PD-FC-9209, National Aeronautical
Laboratory, Bangalore, December 1992.
- S. F. Hoerner, “Fluid-Dynamic Lift Practical Information for Aerodynamic and Hydrodynamic Lift”, 2nd edition, published by Mrs. Liselotte A. Hoernoer, 1985.
- S. F. Hoerner, “Fluid-Dynamic Drag Practical Information for Aerodynamic andHydrodynamic Drag”, 2nd edition, published by Mrs. Liselotte A. Hoernoer, 1985.
- Douglas B. Sweetser, “Doing Physics with Quaternions”, http://quaternions.com
- Paul Jackson, “Jane’s All the World’s Aircraft 2004-2005”, http://Jawa.janes.com.