The “Mass of Control System” in aircraft design refers to the total mass of the components that make up the aircraft’s control system. The control system includes various elements such as control surfaces, control cables, rods, linkages, and actuating mechanisms that are used to control the aircraft’s movement and attitude during flight. Here’s the formula, definition, and SI unit for the Mass of Control System:
Formula for Mass of Control System: The Mass of Control System is determined by measuring the mass of all the components that make up the control system. Mathematically, it can be expressed as:
- Mass of Control System: The total mass of all components in the aircraft’s control system, typically measured in kilograms (kg) or pounds (lb).