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About aircraft
Unmanned aerial vehicle can be termed as a powerd vehicle which carry no human for it's operation, uses aerodynamic force for stability, can fly with weapons, carry lethal or non-lethal payload and can be expandable or recoverable.
Body of Unmanned aerial vehicle
Unmanned aerial vehicle are with absence of cockpit area and windows. Rotary wing UAVs are common form factor of Tailless quadcopters. Crewed platforms are common for tailed mono and bi-copters.
Power source for Unmanned aerial vehicle
lithium polymer battery are used in small Unmanned aerial vehicle where as large Unmanned aerial vehicle required hydrogen fuel cell. Size of the Unmanned aerial vehicle is not defining factor for required energy. Electric power source is also used in Unmanned aerial vehicle as it required less power for operation of flight and it's motor and also they are quieter. An example of electric Unmanned aerial vehicle is Botemite airplane which can climb vertically. For centralized power distribution Battery elimination circuitry (BEC) is used.
Computing
Advance computing technology is required for computing of Unmanned aerial vehicle. Computing gets evolving from analog control to microcontroller and then after system-on-a-chip (SOC) and single-board computers (SBC).
Sensors of Unmanned aerial vehicle
About movement of aircraft, position and movement sensors are responsible to provide information. External information like distance measurements is provided by Exteroceptive sensors. While internal and external states information is provided by exproprioceptive sensors. For separation assurance and collision avoidance, Non-cooperative sensors are used.
Actuators of Unmanned aerial vehicle
To control RPM of motors and to control some digital electronic equipment, digital electronic speed controller is used which is linked to motors/engines and propellers, servomotors, weapons, payload actuators, LEDs and speakers of Unmanned aerial vehicle Actuators.
Good info 👍
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