Remote control (RC) systems form the communication bridge between an RC pilot and their aircraft. Whether you're flying a beginner trainer or a custom FPV aircraft, the transmitter and receiver work together to deliver precise control. In this guide, we’ll cover how RC systems function, break down essential features like channels and signals, and focus on FlySky—a brand known for reliability, affordability, and beginner-friendliness

Learn how airplane control surfaces like ailerons, elevators, and rudders work to steer aircraft. This detailed guide covers their functions, limits, and how RC models use servos, linkages, and transmitter settings for precise control.

The tail section of an airplane plays a critical role in the stability, control, and performance of the aircraft. Whether you're building a foam RC model or designing a full-scale airplane, understanding tail configurations helps you make informed decisions about flight characteristics like yaw control, pitch stability, and aerodynamic efficiency

Dihedral wing design is a foundational element in aircraft stability engineering. By angling the wings upward, designers introduce a natural restoring force that improves roll stability and helps maintain level flight. This makes dihedral ideal for aircraft where ease of control and passive stability are important, such as gliders, UAVs, and training platforms

Wing design is a critical aspect of aerodynamics, influencing how an aircraft generates lift and remains airborne. Whether in birds, aircraft, or drones, the shape, size, and configuration of wings play a vital role in determining their efficiency and performance. This article explores the principles of lift force, how different wing designs impact flight, and key aerodynamic factors engineers consider when designing wings.

Aspect ratio is a fundamental design variable in aircraft engineering. High aspect ratios have aerodynamic efficiency and stable flight characteristics, while low aspect ratios enhance manoeuvrability, structural practicality, and internal space. Engineers must balance these tradeoffs based on the aircraft's intended mission, performance goals, and physical constraints