Fly-By-Wire Technology Term Paper by scribbler

Fly-By-Wire Technology
A review and description of the fly by wire technology in aircraft.
# 153410 | 2,674 words | 7 sources | APA | 2013 | US

$19.95 Buy and instantly download this paper now


The paper discusses the fly by wire technology in aircraft that has replaced the manual flight control with electronic controls. The paper describes the features of fly-by-wire technology and relates that an aircraft designed with fly-by-wire technology is way lighter than an aircraft with a similar design based on conventional manual controls. The paper also discusses how fly-by-wire flight control systems eradicate the intricacy and the weakness of the mechanical circuit of the hydro-mechanical or electromechanical flight control systems. The paper addresses the differences between a digital and analog fly by wire system and discusses the main concern with the digital fly by wire system that is reliability.

From the Paper:

"Fly by wire is a new technology in aircrafts that has replaced the manual flight control with electronic controls. In this technology the flight control signals are converted into electrical signals which are transmitted to the processors through electric wires and the computer determines the movement of the actuators according to the control command (Crane 2002). Moreover, this system sends out certain commands to the computer without any input from the pilot, these commands are mainly transmitted for a more stable flight. The fly-by-wire system also allows automatic signals sent by the aircraft's computers to perform functions without the pilot's input, as in systems that automatically help stabilize the aircraft.
"Mechanical and hydro mechanical flight controls system comprise of all heavy steel cables, metallic pipes with hydraulic fluid, cables and pulleys which adds to the air craft total weight thus slowing it down and decreasing its full efficiency. Both systems frequently need unnecessary backup to tackle mechanical failures, which further increases weight. Additionally, both have inadequate capability to adjust to changing aerodynamic conditions. Dangerous maneuverability such as stalling, spinning and pilot-induced oscillation (PIO), which is dependent chiefly on the strength and configuration of the aircraft concerned rather than the control system itself, can still occur with these systems (Crane 2002)."

Sample of Sources Used:

  • Cran , Dal : Dictionary of A ronautical T rms, third dition, pag 224. Aviation Suppli s & Acad mics, 2002.
  • Dominiqu Brier , Christian Favr , Pascal Trav rs , l ctrical Flight Controls, From Airbus A320/330/340 to Futur Military Transport Aircraft: A Family of Fault-Tol rant Syst ms
  • W. (Spud) Potocki, quot d in Th Arrowh ads, Avro Arrow: th story of th Avro Arrow from its volution to its xtinction, pag s 83-85. Boston Mills Pr ss, rin, Ontario, Canada 2004
  • Whitcomb, Randall L. Cold War T ch War: Th Politics of Am rica's Air D f ns . Apog Books, Burlington, Ontario, Canada 2008.
  • L Tron, X. (2007) A380 Flight Control Ov rvi wPr s ntation at Hamburg Univ rsity of Appli d Sci nc s, 27 S pt mb r 2007

Cite this Term Paper:

APA Format

Fly-By-Wire Technology (2013, May 29) Retrieved March 01, 2024, from

MLA Format

"Fly-By-Wire Technology" 29 May 2013. Web. 01 March. 2024. <>