Modeling and Simulation of Wake Encounter for a Fighter Aircraft

Kamali, C and Pashilkar, AA and Indira, N and Goyal, Anup and Premalatha, and Mudkavi, Vidyadhar Y (2013) Modeling and Simulation of Wake Encounter for a Fighter Aircraft. International Journal of Aerospace Innovations, 4 (3-4). pp. 65-74. ISSN 1757-2258

Full text not available from this repository. (Request a copy)
Official URL: 10.1260/1757-2258.4.3-4.65


This paper addresses the development of six degrees of freedom model for simulation of flight in the wake of a similar class aircraft. The aircraft considered in this study is a high performance fighter with full authority flight control laws. Apart from the aerodynamic effects, the flight dynamic model also includes a model of the air data system and the feedback control laws. The model is used to study the effect of wake on the flight dynamic response of the aircraft with and without effect of wake on the air data system feedback variables like angle of attack, angle of sideslip and static pressure.

Item Type: Article
Uncontrolled Keywords: Fighter aircraft;Flight dynamic model;Aerodynamic effect
Subjects: AERONAUTICS > Aeronautics (General)
Depositing User: Ms. Alphones Mary
Date Deposited: 06 Feb 2014 09:29
Last Modified: 28 Aug 2015 10:19

Actions (login required)

View Item View Item