Volume 20, Issue 1 (7-2001)                   2001, 20(1): 173-187 | Back to browse issues page

XML Persian Abstract Print


Download citation:
BibTeX | RIS | EndNote | Medlars | ProCite | Reference Manager | RefWorks
Send citation to:

M. Bahrami and S. H. Sadati. Minimum-Time Roll Around the Velocity-Vector Maneuver of Aircraft. Journal of Advanced Materials in Engineering (Esteghlal) 2001; 20 (1) :173-187
URL: http://jame.iut.ac.ir/article-1-220-en.html
Abstract:   (5347 Views)
In this paper, some results are provided for minimum time roll about velocity vector maneuvering with thrust-vectoring and aerodynamic control in effect. The mathematical model for attitude motions of the aircraft is developed. First order necessary conditions for optimality using Pontryagen principle is applied, and the existence of an extreme family of solutions for the maneuver is shown. Multiple shooting method is used to obtain the numerical results. An estimate of maneuver time reduction resulting from thrust-vectoring is obtained. Keywords: Multiple Shooting Method Minimum time Thrust-Vectoring Maneuverability Aerodynamics
Full-Text [PDF 300 kb]   (1337 Downloads)    
Type of Study: Research | Subject: General
Received: 2014/10/25 | Published: 2001/07/15

Add your comments about this article : Your username or Email:
CAPTCHA

© 2024 CC BY-NC 4.0 | Journal of Advanced Materials in Engineering (Esteghlal)

Designed & Developed by : Yektaweb