Ingenieur Vol 80 ingenieur 2019 octoberfinal | Page 46

INGENIEUR Systematic UAV Design By Shuhaimi Mansor Professor in Flight Dynamics Wan Zaidi Wan Omar Senior Lecturer in Aircraft Design Universiti Teknologi Malaysia U nmanned Aerial Vehicles (UAVs) are flying machines that can be automatically controlled and navigated without aircrew on board. UAVs are also commonly known as drones. An Unmanned Aircraft System (UAS) however is a system which includes a flying machine, a ground-based control and monitoring system and the communication system between the two. Many years ago, we might have heard of UAVs or drones used in dangerous and expensive military applications, but nowadays we can buy one from hobby shops or even build one of your own. The price of a drone varies from a few thousands to millions of dollars, depending on their performances (which are mainly speed, altitude and endurance), functionality, capability and payloads. The general configuration of the UAVs can be divided into three types: fixed-wing, rotor-craft or combination of the two. The general public, particularly in Malaysia, is already widely exposed to very small, lightweight UAVs. Most of them fall into micro UAV (MUAV) category, with limited operation, for personal use, fly within line of sight for taking photos, videos and recreational purposes. Due to the popularity of the quad-copter configuration, the public has largely accepted that the multi-rotor UAV is a “drone”. In contrast, there are UAVs with the size of an airline jets such as the Boeing 737 capable of a flying range of hundreds of km and more than 24 hours endurance. They can cruise at altitudes of more than 40,000 ft and are capable to fly during the day and/or night. 6 44 VOL 2019 VOL 80 55 OCTOBER-DECEMBER JUNE 2013 UAV Mission Requirements UAV applications cover a wide range from personal use and civil commercial use such as aerial photography, aerial surveillance, to military applications such as carriage of guided missile, rockets and aerial intelligence. The application of UAVs started as early as World War II in the form of the V1 and V2 rockets by Germany. Then came the surveillance systems where Israeli “aircraft without pilots” were reported shot down over Egypt in the Yom Kippur war. Many more applications came about after these military uses. Cheaper systems, which are more and more electronic-based modern instrumentation and control systems became easily available as did payloads like cameras and the communication systems. Any data collected in a flight could be directly transmitted to the controls on the ground, enabling the flying platform to continue flying and continue to collect data. All these enable high rates of utility and cheaper operation. UAVs can be classified into several categories. These categories are grouped by size, weight, range, endurance and cruising altitudes. Figure 1 gives an idea of the classes of current UAVs in the market, based on the range-altitude capabilities of UAVs. Micro UAV (MUAV) covers the low end of the market, with maximum take-off weight of less than five kg. MUAVs can be built without going through a comprehensive knowledge in aerodynamics, stability and controls. Most of the parts required to