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Drone Development from Concept to Flight
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As we have gone through use cases that are catered for by the use of drone technology, here, we will study different types of drones that have been built for the sake of different application requirements such as high endurance, long range, high altitude, and so on. By doing this, we will get to know about the different kinds of drones and later build an understanding of their development. A glimpse at various kinds of drones is covered in the following section.
In this section, we will study the various types of drones, their key functionality, and how they are different from each other.
A multirotor is a motor-propeller-based drone. The major elements to produce force and lift in the air are motors and propellers attached to them. This produces thrust in the drone and helps to lift the system’s load.
Based on the number of motors, these drones are classified as follows:
Figure 1.1 – A bi-copter
Figure 1.2 – A tri-copter
Figure 1.3 – A quadcopter
Figure 1.4 – A hexacopter
Figure 1.5 – An octocopter
Figure 1.6 – An octa-quad
Figure 1.7 – A deca-hexa copter
The preceding configuration is used as per the decided payload, load-carrying capacity, and applications.
A fixed-wing drone, as the name suggests, is a standard airfoil wing-based design where the wing serves as a key lift generator for the system and a single motor (push/pull) helps to cruise in the air. The cruise speed helps to generate adequate lift via wings to travel in the air, and control surfaces work to give direction in the air:
Figure 1.8 – A fixed-wing drone
Vertical take-off and landing (VTOL) aircraft, also called hybrid aircraft, is assisted by four motors to lift off in the air and later transition into a fixed-wing aircraft. This type of drone does not require a long runway unlike fixed-wing drones. It take off and land like a multicopter from a single place and cruises like a fixed-wing aircraft:
Figure 1.9 – A fixed-wing VTOL
A tilt-rotor drone comes under the category of fixed-wing VTOL hybrid drones that take off and land like a multirotor and cruise like a fixed-wing drone. The only difference between these drones and fixed-wing VTOL drones is that these drones work on the principle of differential thrust and have common motors for cruise and take-off. The same motors are used as take-off lifter motors, change their angle from 90 degrees to 180 degrees during transition, and are used as cruise motors.
These drones give much more efficiency than a fixed-wing VTOL since the number of motors is reduced and power consumption is also reduced:
Figure 1.10 – A tilt-rotor hybrid drone
Hence, we have seen different types of drones. These drones can be built in different weight and size categories, but to differentiate them based on their weight profile, the Directorate General of Civil Aviation (DGCA) in India has classified drones into five categories:
We have now studied different types of drones based on their structure and application, but we haven’t yet studied what’s actually inside the drone and the systems it contains. In the following sections, we will understand the composition of a drone and bifurcate it into different categories.
A UAV has many systems and subsystems that enable it to fly in the air and do missions automatically with safety and precision. These systems are a combination of hardware and software that perform their respective tasks to keep the system under control and stable in the air:
Figure 1.11 – Overview of a drone system
Now that we have seen the system composition of a UAV, let us look at the major mechanical and structural components of drones.
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