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nptel drone week 1

Total questions: 40

Worksheet time: 20mins

Name
Class
Date
1.

What is a key advantage of fixed-wing drones over multirotor drones?

a)

Vertical take-off

b)

Longer flight duration

c)

Stable hovering

d)

Easier control for beginners

2.

In a hybrid VTOL drone, which mechanism allows it to switch from vertical lift to forward flight?

a)

Tilt-rotor system

b)

Balloon inflation system

c)

Swashplate actuator

d)

Magnetic rotor coupling

3.

In drone terminology, what is a “failsafe” feature?

a)

A backup battery

b)

An emergency parachute

c)

A system that safely returns the drone home if signal is lost

d)

A GPS booster for better navigation

4.

What is geofencing in drone operations?

a)

A technique to protect propellers from damage

b)

A method to prevent drones from flying into restricted zones

c)

A system to guide drones using magnetic fields

d)

A feature for stabilizing drones during windy conditions

5.

What provides lift to a multirotor drone like a quadcopter?

a)

Fixed wings

b)

Rotating blades (propellers)

c)

Balloon mechanism

d)

Gliding motion

6.

Why are counter-rotating propellers used in quadcopters?

a)

To increase the speed

b)

To reduce battery consumption

c)

To cancel out rotational torque

d)

To boost vertical thrust

7.

Which aerodynamic principle explains lift generation in drone propellers?

a)

Newton’s First Law

b)

Bernoulli’s Principle

c)

Archimedes’ Principle

d)

Hooke’s Law

8.

What happens when all propellers of a quadcopter rotate in the same direction?

a)

The drone flies faster

b)

The drone hovers more stably

c)

The drone starts spinning uncontrollably

d)

The drone saves power

9.

In drone flight dynamics, rotational motion about the drone's longitudinal axis is referred to as:

a)

Pitch

b)

Roll

c)

Yaw

d)

Surge

10.

A quadcopter in a hover experiences no net translation because:

a)

All thrust vectors cancel each other out

b)

All propellers rotate in the same direction

c)

The net force equals zero and torque equals zero

d)

Its moment of inertia is infinite

11.

If a drone’s center of mass shifts due to payload, which aspect of its rigid body motion is most directly affected?

a)

Linear acceleration only

b)

Angular velocity distribution

c)

Moment of inertia and dynamic stability

d)

Rotor torque profile remains unchanged

12.

During a pitch maneuver (nose up), what type of motion is primarily occurring?

a)

Translation in the X-direction

b)

Rotation about the lateral axis

c)

Rotation about the vertical axis

d)

Translation in the Z-direction

13.

Which of the following actions would cause pure translation in a drone (no rotation)?

a)

Increasing speed of diagonal rotors

b)

Equal thrust increase in all four rotors

c)

Spinning two opposite rotors faster

d)

Tilting the drone via asymmetric thrust

14.

Why is the moment of inertia crucial in drone attitude control?

a)

It determines the battery consumption

b)

It controls air resistance

c)

It affects torque required for rotational acceleration

d)

It is used only for altitude holding

15.

A drone performs a coordinated turn (banked yaw with no lateral slip). Which type of motion best describes this?

a)

Rigid body translation

b)

Pure yaw

c)

Coupled translation and rotation

d)

Independent axis motion

16.

Which part of a drone converts electrical energy into mechanical thrust?

a)

Flight controller

b)

Electronic Speed Controller

c)

BLDC motor

d)

GPS module

17.

What is the main function of the flight controller in a UAV?

a)

Generate lift

b)

Stabilize and control the drone

c)

Supply power to the ESC

d)

Store flight footage

18.

The key parameter that affects the drone’s endurance is:

a)

Propeller pitch

b)

Battery capacity

c)

Motor Kv rating

d)

Airframe color

19.

The lift generated by drone propellers depends on:

a)

Propeller speed and air density

b)

ESC firmware version

c)

Type of GPS module

d)

Battery connector

20.

Which sensor measures angular velocity for drone stabilization?

a)

Barometer

b)

Gyroscope

c)

Magnetometer

d)

GPS

21.

The accelerometer in a drone helps to detect:

a)

Rotational motion

b)

Linear acceleration

c)

GPS position

d)

Motor temperature

22.

Which of the following is a limitation of multirotor drones?

a)

Low maneuverability

b)

Shorter flight duration

c)

Low control precision

d)

Heavy payload capacity

23.

What type of drone uses flapping-wing motion similar to birds?

a)

Rotary-wing

b)

Fixed-wing

c)

Ornithopter

d)

VTOL

24.

The aerodynamic drag on a drone increases with:

a)

Decrease in airspeed

b)

Increase in airspeed

c)

Constant altitude

d)

Low thrust

25.

In drone dynamics, yaw is rotation about the:

a)

Longitudinal axis

b)

Vertical axis

c)

Lateral axis

d)

Roll axis

26.

The pitch motion of a quadcopter is controlled by changing the speed of:

a)

All four rotors equally

b)

Front and rear rotors

c)

Left and right rotors

d)

Diagonal rotors

27.

The roll motion in a quadcopter is generated by varying thrust between:

a)

Front and rear rotors

b)

Left and right rotors

c)

All rotors equally

d)

Only rear rotors

28.

What is the typical operating frequency for GPS modules in drones?

a)

1.575 GHz

b)

2.4 GHz

c)

900 MHz

d)

433 MHz

29.

Which component controls the rotational speed of a BLDC motor?

a)

Battery

b)

ESC

c)

Flight controller

d)

Receiver

30.

The torque of a BLDC motor increases with:

a)

Higher current

b)

Lower voltage

c)

Higher frequency

d)

Reduced propeller diameter

31.

What is the main role of the Electronic Speed Controller (ESC)?

a)

Convert DC to AC for BLDC motors

b)

Stabilize the flight attitude

c)

Measure propeller thrust

d)

Control camera movement

32.

Which type of battery is most commonly used in UAVs?

a)

NiMH

b)

LiPo

c)

Lead-acid

d)

NiCd

33.

The C-rating of a LiPo battery represents:

a)

Total capacity

b)

Maximum safe discharge rate

c)

Number of cells

d)

Battery weight

34.

A drone’s flight time can be increased by:

a)

Increasing payload

b)

Reducing weight and improving propeller efficiency

c)

Using smaller ESCs

d)

Reducing motor RPM

35.

During take-off, the thrust generated must be:

a)

Equal to the drone’s weight

b)

Greater than the drone’s weight

c)

Less than the drone’s weight

d)

Half of the drone’s drag

36.

The PID controller in a flight control system adjusts:

a)

Rotor blade pitch

b)

Motor speed to maintain stability

c)

Battery voltage

d)

Camera angle

37.

The “D” term in a PID controller is used to:

a)

Measure steady-state error

b)

Predict future error

c)

Eliminate offset

d)

Increase proportional gain

38.

The GPS module in a drone helps in:

a)

Attitude estimation

b)

Position and navigation

c)

Power management

d)

Communication between ESCs

39.

Which sensor helps the drone maintain altitude by measuring air pressure?

a)

Magnetometer

b)

Barometer

c)

Gyroscope

d)

Thermometer

40.

In a quadcopter, what ensures stability during hover?

a)

Equal thrust from all motors

b)

Higher thrust from front motors

c)

Increased yaw rate

d)

Reduced roll