Feb 9, 2020

Posted by in Business and Finance | 0 Comments

This Is What People Must Know About Flight Control System

This Is What People Must Know About Flight Control System

Flight Control System is used to control the effect of force (force) on an aircraft, the direction (direction) of flying and the attitude (attitude) of an aircraft. It should be noted that the flight steering control system and its characteristics can vary depending on the type of aircraft. Most basic designs of the fly steering control system are mechanical. The operating system combines mechanical parts such as rods, cables, pulleys, and chains to continue the force from the flying control column to the aircraft control device. Mechanical control systems are currently still used in small aircraft and sports aircraft categories where the aerodynamic force is not too excessive. Besides that, before we continue, if your airplane FBW’s ball screws are broken, we recommend you to take them to the best related site company near your hangar.

Flight Control System consists of two systems, namely:

1. The primary control system and,
2. Secondary control system.

The main control system as known as Primary Control System consists of:

1. Aileron,
2. Elevators and,
3. Rudder.

All three are the main control system and are used to control the aircraft to be safe and well-controlled during flight.

The secondary control system consists of:

1. Wing flaps,
2. Leading-edge,
3. Spoilers and,
4. Trim the system.

Used to improve the performance characteristics of an aircraft or alleviate excessive control forces on an aircraft’s steering.

Primary Flight Control

The aircraft control system is designed to provide adequate response to control inputs that allow natural feel. At very low speeds, control usually feels soft and slow, and the reaction plane is slow to control. At very high speeds, control becomes stronger and the response of the aircraft is faster.

Movement of one of the three main flight steering controls (ailerons, elevators or rudder), changes the airflow and distribution pressure over and around the airfoil. This change affects the lift and drag forces produced by a combination of airfoil/steering control and allows the pilot to control the aircraft on all three axes of rotation.

The flight control surfaces deflection design feature is limited in size, the purpose of this design restriction is to prevent pilots from accidentally overcontrolling and overstressing aircraft during normal maneuvers.