Hostname: page-component-cd9895bd7-jkksz Total loading time: 0 Render date: 2024-12-26T16:34:18.550Z Has data issue: false hasContentIssue false
  • English
  • Français

Some analytical and numerical solutions for the safe turn manoeuvres of agricultural aircraft – an overview

Published online by Cambridge University Press:  03 February 2016

B. Rasuo
B. Rasuo*
Affiliation:
University of Belgrade Belgrade, Yugoslavia
Get access Rights & Permissions [Opens in a new window]

Abstract

In this paper, a theoretical study of the turn manoeuvre of an agricultural aircraft is presented. The manoeuvre with changeable altitude is analyzed, together with the, effect of the load factors on the turn manoeuvre characteristics during the field-treating flights. The mathematical model used describes the procedure for the correct climb and descent turn manoeuvre. For a typical agricultural aircraft, the numerical results and limitations of the climb, horizontal and descending turn manoeuvre are given. The problem of turning flight with changeable altitude is described by the system of differential equations which describe the influence of the normal and tangential load factors on velocity, the path angle in the vertical plane and the rate of turn, as a function of the bank angle during turning flight. The system of differential equations of motion was solved on a personal computer with the Runge-Kutta-Merson numerical method. Some analytical and numerical results of this calculation are presented in this paper.

Type
Research Article
Information
The Aeronautical Journal , Volume 111 , Issue 1123 , September 2007 , pp. 593 - 599
Copyright
Copyright © Royal Aeronautical Society 2007 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Etkin, B. and Reid, L.D., Dynamics of Flight, 1996, 3rd ed, John Wiley & Sons, New York, pp 238–242.Google Scholar
2. Mair, W.A. and Birdsall, D.L., Aircraft Performance, 1996, (Reprint), Cambridge University Press, pp 214–236.Google Scholar
3. Vinh, N.X.. Flight Mechanics of High Performance Aircraft, 1999, (Reprint), Cambridge University Press, pp 221–252.Google Scholar
4. Phillips, W.F., Mechanics of Flight, John Wiley & Sons Inc, Hoboken, New Jersey, 2004, pp 281–299, 804–819.Google Scholar
5. Filippone, A., Flight Performance of Fixed and Rotary Wing Aircraft, 1st ed, Elsevier, 2006, Oxford, pp 251–265.Google Scholar
6. Kutschera, A. and Render, P.M.. Corner speed versus optimum turn speed, Aeronaut J, July 2003, 107, (1073), pp 443–445.Google Scholar
7. American National Standard, Recommended Practice for Atmospheric and Space Flight Vehicle Coordinate Systems, ANSI/AIAA R-004-1992, Washington, USA.Google Scholar
8. Gajic, D. and Rasuo, B.. Effects of load factors on the first phase turn characteristics during the agricultural flights, Tehnika, 1982, 31, (12), pp 1881–1882, 1890 (in serbian).Google Scholar
9. Rasuo, B.. Analytic solution of the calculation of turn manoeuvre of agricultural aircraft, The JSASS 14th International Sessions in 38th Aircraft Symposium, 2000, Sendai, Japan, pp 669–672.Google Scholar
10. Rasuo, B.. Effects of load factors on turn manoeuvre of agricultural aircraft, 1998, 21st ICAS Meeting Papers on Disc [CD-ROM], Melbourne, Australia.Google Scholar
11. Rasuo, B.. Analytical and numerical modeling of the turn manoeuvre of agricultural aircraft, 2001 World Aviation Congress Papers on Disc [CD-ROM], 2001, Seattle, Washington, USA.Google Scholar
12. ICL Scientific Subroutines, Mathematics Subroutines, part 1, 1995, Software Package, London, UK.Google Scholar