China Civil UAV Theory Questions — Questions 296–305

Unofficial study reference only. Not affiliated with or endorsed by any civil aviation authority — the official syllabus and regulations prevail.

0 / 10

UAV-Q0296. The main reason multi-axis aircraft power units are mostly electric is

Explanation

A multi-axis aircraft performs its maneuvers by adjusting each rotor's speed. A fuel engine would need a gearbox to change speed, which responds slowly. An electric system only needs to adjust current to change motor speed quickly, with a simple structure and fast response.

UAV-Q0297. The flight control computer of a multi-axis aircraft does NOT

Explanation

Receiving ground control signals is the function of the onboard remote receiver.

UAV-Q0298. The device that directly controls multi-axis aircraft motor speed is

Explanation

The ESC's full name is electronic speed controller (Electronic Speed Control), abbreviated ESC. Depending on the drive motor, ESCs are brushed or brushless. The ESC regulates motor speed according to the control signal. The flight controller sends control signals to the ESC, controlling motor speed indirectly; the device that controls speed directly is the ESC.

UAV-Q0299. Structurally, a multi-axis aircraft propeller is closer to

Explanation

Wind turbines and helicopter rotors can change pitch; fixed-wing airplane and multi-axis propellers use fixed-pitch propellers.

UAV-Q0300. On each “axis” of a multi-axis aircraft, there is generally

Explanation

One ESC connects to one motor.

UAV-Q0301. The normal signal flow on a multi-axis aircraft is

Explanation

Study note: receiver first, then flight controller. The onboard remote receiver receives the signal and passes the command to the flight controller for processing; the flight controller then sends the processed commands to each ESC, and each ESC controls its motor's speed.

UAV-Q0302. A multi-axis aircraft link antenna should be installed _______ the flight controller and GPS antenna

Explanation

The link antenna frequently receives and sends information, so to avoid interfering with the flight controller and GPS it must be kept away from the flight controller and GPS antennas.

UAV-Q0303. Multi-axis aircraft ESCs are usually classified as

Explanation

ESCs are brushed or brushless. Motors are classified as DC/AC, brushed/brushless, and outrunner/inrunner/stepper. Multi-rotor UAVs typically use a brushless ESC driving a three-phase AC outrunner brushless motor.

UAV-Q0304. The ESC generally used on multi-axis aircraft is

Explanation

A brushless ESC is an electronic device that controls a brushless motor's speed and direction. Multi-axis aircraft motors are generally brushless, so brushless ESCs are used.

UAV-Q0305. The power battery generally used on multi-axis aircraft is

Explanation

Li-polymer batteries have high energy density: for the same capacity, a lithium battery is the lightest in weight.