You are here:

Fighter Pilot Ejection Study as an Educational Tool
ARTICLE

,

TMIAAIJI Volume 29, Number 4, ISSN 0268-3679

Abstract

In this article, we apply the well-known equations of projectile motion to the case of a fighter pilot ejecting from an aircraft, the aim being to establish under what conditions there is danger of impact with the rear vertical stabilizer. The drag force on the pilot after ejection is assumed to vary as the velocity squared and the aircraft motion is assumed to be confined to a plane (i.e. roll, yaw and pitch are not included), but it is not restricted to horizontal flight. The study is, however, limited to the case of no propulsion force acting on the pilot after ejection, as is appropriate to the older style of ejection seat. The problem has been coded in MATLAB and some illustrative numerical results are presented. We envisage that student interest in the numerical solution of differential equations will be stimulated by this application of projectile motion to an interesting real-life and potentially life-threatening situation.

Citation

Robinson, G. & Jovanoski, Z. (2010). Fighter Pilot Ejection Study as an Educational Tool. Teaching Mathematics and Its Applications: An International Journal of the IMA, 29(4), 176-192. Retrieved January 19, 2020 from .

This record was imported from ERIC on April 19, 2013. [Original Record]

ERIC is sponsored by the Institute of Education Sciences (IES) of the U.S. Department of Education.

Copyright for this record is held by the content creator. For more details see ERIC's copyright policy.

Keywords