Aircraft Structures and Control
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Subject: Aviation And Aerospace Engineering
Class: SHS 2
Term: 2nd Term
Week: 1
Grade code: 3.1.3.LI.3
Strand code: 1
Sub-strand code: 3
Content standard code: 3.1.3.CS.2
Indicator code: 3.1.3.LI.3
Theme: Core Concepts in Aerospace Engineering
Subtheme: Aircraft Structures and Control
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This lesson moves our focus from the atmosphere to the vacuum of space. While we have learned how aeroplanes use wings, rudders, and elevators to control their movement by pushing against the air, spacecraft operate in an environment where there is no air to push against. This topic is highly relevant to our lives in Ghana. Many services we use daily—from watching DSTV or GOtv, to using Google Maps on our phones, to receiving weather forecasts for farming—depend on satellites orbiting the Earth. These satellites must be able to control their orientation, or "attitude," to point their antennas, cameras, and sensors in the right direction.
A. The Fundamental Problem: Control in a Vacuum
The first and most important concept to understand is the environment of space. It is a near-perfect vacuum, meaning it is empty of matter. There is no air. Aircraft Control: An aeroplane turns by using its control surfaces (ailerons, rudder, elevator) to deflect air. The force of the air pushing against these surfaces causes the aircraft to rotate. Spacecraft Control: In a vacuum, there is no air to push against. Therefore, a spacecraft's rudder or wings would be completely useless for changing its orientation.
This means spacecraft need entirely different mechanisms to control their attitude.
> Attitude: The orientation of an object in space. For a spacecraft, this refers to its pitch (nosing up/down), yaw (nosing left/right), and roll (rotating along its main axis). Controlling the attitude is called Attitude Control. B. Major Types of Spacecraft Control Mechanisms (Active Systems)