Untitled Quiz
61 Questions
0 Views

Choose a study mode

Play Quiz
Study Flashcards
Spaced Repetition
Chat to Lesson

Podcast

Play an AI-generated podcast conversation about this lesson

Questions and Answers

What aspect of design did Wilbur Wright suggest was easier for helicopters compared to airplanes?

  • Efficiency in labor
  • Design complexity (correct)
  • Cost-effectiveness
  • Safety features

Which inventor is associated with the development of the tail rotor in helicopters?

  • Cierva
  • Boris Yurev (correct)
  • Elmer Sperry
  • Igor Sikorsky

What significant device did Elmer Sperry contribute to the field of helicopter design?

  • Proximity sensor
  • Gyroscope (correct)
  • Autopilot system
  • Tail rotor

What was the year of the first unmanned helicopter developed by Igor Sikorsky?

<p>1909 (B)</p> Signup and view all the answers

Which UAV was introduced first in the modern era?

<p>RQ-8A Fire Scout (A)</p> Signup and view all the answers

What type of experiments related to unmanned helicopters were mentioned in the content?

<p>LARICS experiments (D)</p> Signup and view all the answers

What year did Cierva contribute to helicopter development?

<p>1923 (C)</p> Signup and view all the answers

What kind of physical interactions do aerial vehicles have with their environment in unmanned operations?

<p>Environmental adaptability (B)</p> Signup and view all the answers

What are the key components of 6 degrees of freedom (6 DOF) for UAVs?

<p>X, y, z, roll, pitch, yaw (C)</p> Signup and view all the answers

Why are UAVs described as underactuated systems?

<p>They have fewer controls than degrees of freedom. (D)</p> Signup and view all the answers

What does the term 'coupled' refer to in the context of UAV systems?

<p>Each movement affects the others. (B)</p> Signup and view all the answers

What does 'neutral buoyancy' imply for a blimp?

<p>The blimp will remain at a constant altitude. (A)</p> Signup and view all the answers

In which coordinate system is the body frame {B} positioned relative to?

<p>The world frame {W} (D)</p> Signup and view all the answers

What are the effects of UAVs being nonlinear systems?

<p>Small changes in inputs can lead to large changes in outputs. (B)</p> Signup and view all the answers

Which frame is typically the starting point for helicopter operations?

<p>The world frame {W} (C)</p> Signup and view all the answers

Which mathematical expression is used to describe transforms in UAV systems?

<p>C = cos(?), S = sin(?) (D)</p> Signup and view all the answers

What does the equation $I \cdot \theta{\ddot{}} = \tau_{uz\alpha} - \tau_{\mu y} - \tau_{tr} - \tau_{Dy} + \tau_{G}$ represent?

<p>The motion dynamics in the x-z plane (pitch) (C)</p> Signup and view all the answers

Which torque acts against the main rotor's torque in the roll motion equation?

<p>Friction torque (B)</p> Signup and view all the answers

In the context of a helicopter's swash plate mechanism, what does the swash plate torque primarily affect?

<p>Roll control (B)</p> Signup and view all the answers

What does the symbol $\tau_{tr}$ represent in the motion equations of a helicopter?

<p>Tail rotor drag torque (D)</p> Signup and view all the answers

Which variable in the equations represents the angular acceleration in the roll motion?

<p>$\phi{\ddot{}}$ (A)</p> Signup and view all the answers

What do the terms $\tau_{ux\beta}$ and $\tau_{\mu x}$ represent in the helicopter's roll dynamics?

<p>Torque inputs for roll control (A)</p> Signup and view all the answers

In the roll equation $I \cdot \phi{\ddot{}} = \tau_{uz\beta} - \tau_{\mu x} - \tau_{Dx}$, what does $\tau_{Dx}$ indicate?

<p>Drag torque (C)</p> Signup and view all the answers

Which factor does gyroscopic torque primarily influence in a helicopter model?

<p>Response to roll and pitch changes (B)</p> Signup and view all the answers

What primary function does the IMU serve in a UAV system?

<p>Position and motion sensing (A)</p> Signup and view all the answers

Which of the following is NOT a component of the UAV's hardware configuration?

<p>Environmental Shielding (C)</p> Signup and view all the answers

What role does the Kalman filter play in the UAV's sensor system?

<p>To eliminate position drift (C)</p> Signup and view all the answers

Which component is responsible for maintaining the UAV's speed measurements?

<p>GPS (C)</p> Signup and view all the answers

What is indicated by the factor $\lambda_i$ when analyzing rotor performance?

<p>Induced speed ratio (B)</p> Signup and view all the answers

What technology is required for communication between the UAV and its ground control?

<p>Wireless Modem (D)</p> Signup and view all the answers

What is the function of the D-GPS in the UAV configuration?

<p>To refine positioning accuracy (C)</p> Signup and view all the answers

What does the equation $C_L = 2\pi\alpha_e$ calculate in relation to propellers?

<p>Lift coefficient (A)</p> Signup and view all the answers

Which sensor measures the angular velocity of the UAV during flight?

<p>Gyro (C)</p> Signup and view all the answers

In analyzing the thrust produced by a propeller, which of the following factors is most critical?

<p>Rotational speed of the propeller (A)</p> Signup and view all the answers

Which of the following systems provides data necessary for controlling a UAV's flight dynamics?

<p>R-1 Integrated Avionics System (C)</p> Signup and view all the answers

What effect does vertical motion have on the thrust generated by a propeller?

<p>It reduces the effective angle of attack. (B)</p> Signup and view all the answers

Which variable is used to quantify the drag force on a propeller during its operation?

<p>Torque constant (A)</p> Signup and view all the answers

What is the primary use of the motion pack in the UAV's sensor suite?

<p>For inertial motion sensing (B)</p> Signup and view all the answers

What type of sensor is primarily responsible for detecting the UAV's position relative to Earth?

<p>GPS (D)</p> Signup and view all the answers

The stall torque of a DC motor refers to what scenario?

<p>Maximum load capacity without rotating (B)</p> Signup and view all the answers

What does the variable $\Omega R$ denote in propeller operations?

<p>Angular velocity of the rotor (B)</p> Signup and view all the answers

During aerial manipulation, what is the impact of back electromagnetic force on a DC motor?

<p>It decreases torque output. (C)</p> Signup and view all the answers

What is the significance of the term $\Theta_0$ in rotor performance equations?

<p>It is the mechanical angle at ¾ R. (B)</p> Signup and view all the answers

Which parameter affects the effective angle of attack according to horizontal motion dynamics?

<p>Angle of inclination (B)</p> Signup and view all the answers

Which condition describes vertical motion when $V_{xy} = 0$ and $V_c = 0$?

<p>All thrust generated is vertical. (D)</p> Signup and view all the answers

Which equation primarily determines thrust based on rotor dynamics?

<p>$T = \rho V^2 C_L A$ (B)</p> Signup and view all the answers

What can be concluded about the relationship between power and torque in a DC motor?

<p>Power is proportional to voltage and torque. (A)</p> Signup and view all the answers

Which factor primarily influences the translational motion of a multirotor UAV?

<p>Thrust produced by propulsors (D)</p> Signup and view all the answers

What defines the mapping of how propulsors are attached to a multirotor for independent control?

<p>Configuration mapping Γ (A)</p> Signup and view all the answers

Which orientation describes the relationship between the body frame and the world frame in a UAV model?

<p>Position and orientation (B)</p> Signup and view all the answers

What was a significant technological advancement in the first quadcopter developed at FER in 2006?

<p>Utilization of mechanical gyros (C)</p> Signup and view all the answers

Which type of rotation is associated with the operation of propulsors in a multirotor?

<p>Clockwise (CW) and counterclockwise (CCW) rotation (A)</p> Signup and view all the answers

What motion does the drag produced by propulsors primarily affect in a UAV?

<p>Rotational motion (D)</p> Signup and view all the answers

What is the primary role of the thrust produced by an individual propulsor?

<p>To maintain altitude (A)</p> Signup and view all the answers

In UAV control, what is one main characteristic of rotational motion?

<p>Determined by drag forces (B)</p> Signup and view all the answers

What does DOF stand for in the context of UAV control systems?

<p>Degree of Freedom (B)</p> Signup and view all the answers

Which representation is used to describe the orientation of the UAV's body frame concerning the world frame?

<p>Orientation angles (B)</p> Signup and view all the answers

Which of the following best describes the behavior of multirotor UAVs under mechanical gyro influences?

<p>Enhanced stability (C)</p> Signup and view all the answers

What is likely to happen if the propulsors on a multirotor are not configured using mapping Γ?

<p>Difficulties in independent control (C)</p> Signup and view all the answers

What aspect of UAV control is predominantly influenced by torque produced by propulsors?

<p>Rotational axis control (C)</p> Signup and view all the answers

What is a primary requirement for effective multirotor motion control?

<p>Simultaneous adjustment of thrust and drag (B)</p> Signup and view all the answers

Flashcards

Helicopter vs. Airplane Design

The helicopter is easier to design than the airplane, but its practical use is often limited.

Early Helicopter Developments (1909-1916)

Significant progress in the early 20th century included unmanned helicopters, tail rotors, and gyroscope applications.

Post-WWI Helicopter Design

New helicopter designs emerged after World War I, prominently by Cierva and Sikorsky, marking a phase of advancing technology.

Modern Era Unmanned Helicopters

Later innovations include unmanned helicopters like the RQ-8A Fire Scout and Schiebel CAMCOPTER, showcasing advancements in technology.

Signup and view all the flashcards

Environment and Aerial Vehicles (Manned)

This section focuses on how manned aerial vehicles interact with the environment.

Signup and view all the flashcards

Environment and Aerial Vehicles (Unmanned)

This part focuses on how unmanned aerial vehicles interact with the environment.

Signup and view all the flashcards

Predictions on UAV Autonomy (1985)

Future predictions about the autonomous capabilities of unmanned aerial vehicles (dating back to 1985).

Signup and view all the flashcards

LARICS Experiments

Research experiments on the interaction between aerial vehicles and the surrounding environment, possibly encompassing manned and unmanned vehicles.

Signup and view all the flashcards

UAV Degrees of Freedom

A UAV has 6 degrees of freedom (DOF): x, y, z position and roll, pitch, yaw orientation.

Signup and view all the flashcards

UAV System Characteristics

UAV systems are nonlinear, multivariable, coupled, and underactuated, making them complex to control.

Signup and view all the flashcards

Body Frame {B}

A frame of reference attached to the UAV's body.

Signup and view all the flashcards

World Frame {W}

The frame of reference that describes the environment.

Signup and view all the flashcards

Mathematical Models (UAVs)

Equations used to represent a UAV's movement and behaviour.

Signup and view all the flashcards

Coordinate Transformations

Methods for changing between different reference frames (like body and world frames).

Signup and view all the flashcards

Blimp Math Model

Equations describing a blimp's movement; often involving position and orientation elements.

Signup and view all the flashcards

Neutral Buoyancy

A condition where an object neither sinks nor floats.

Signup and view all the flashcards

Helicopter Roll

The rotation of a helicopter around its longitudinal axis (x-axis).

Signup and view all the flashcards

Helicopter Pitch

The rotation of a helicopter around its lateral axis (y-axis).

Signup and view all the flashcards

Swash Plate Torque

The force applied by the swash plate, controlling the main rotor's pitch and thus the helicopter's lift and direction.

Signup and view all the flashcards

Gyroscopic Torque

A torque caused by the spinning main rotor, resisting changes in its orientation. This influences the helicopter's roll and pitch.

Signup and view all the flashcards

Friction Torque

The resisting force due to friction between moving parts in the helicopter, impacting its rotation.

Signup and view all the flashcards

Tail Rotor Drag Torque

The resistance created by the tail rotor as it spins, counteracting the torque of the main rotor and keeping the helicopter from spinning in the opposite direction.

Signup and view all the flashcards

Gravity Torque

The force of gravity acting on the helicopter, pulling it down.

Signup and view all the flashcards

What are the main factors affecting helicopter rotation?

The primary forces influencing helicopter rotation include swash plate torque (controlling lift/direction), gyroscopic torque (resisting changes), friction torque (resisting motion), tail rotor drag torque (counteracting spin), and gravity torque (pulling it down).

Signup and view all the flashcards

UAV Sensors

Devices that gather information about the environment surrounding the UAV, such as obstacle locations, target presence, or weather conditions.

Signup and view all the flashcards

Sensor Fusion

The process of combining information from multiple sensors to create a more accurate and comprehensive understanding of the environment.

Signup and view all the flashcards

IMU (Inertial Measurement Unit)

A sensor that measures the UAV's acceleration, rotation, and magnetic field orientation.

Signup and view all the flashcards

GPS (Global Positioning System)

A satellite-based system used to determine the UAV's precise location on Earth.

Signup and view all the flashcards

IMU Position Drift

A gradual error in the IMU's position estimation over time, caused by sensor inaccuracies.

Signup and view all the flashcards

On Board System

The core of the UAV, consisting of its computer, sensors, and flight control processor.

Signup and view all the flashcards

Flight Control Processor

The computer responsible for controlling the UAV's flight path and stability.

Signup and view all the flashcards

Control Actuators

Mechanical components that move the UAV's control surfaces, changing its direction and attitude.

Signup and view all the flashcards

Ground Station

The base of operations for the UAV, containing equipment for controlling, monitoring, and communicating with it.

Signup and view all the flashcards

Mission Control Station

A specific part of the ground station, where the mission is planned and executed.

Signup and view all the flashcards

Multirotor Configuration Mapping (Γ)

The arrangement of propulsors on a multirotor body that ensures independent control of all degrees of freedom (DOFs).

Signup and view all the flashcards

Degrees of Freedom (DOFs)

The independent directions in which a body can move or rotate.

Signup and view all the flashcards

Multirotor Body Frame (B)

A coordinate system attached to the multirotor's body, used to define its orientation and position.

Signup and view all the flashcards

Propulsors in Multirotor

The motors and propellers that generate the thrust and torque for a multirotor's flight.

Signup and view all the flashcards

Translational Motion in Multirotors

Movement of the multirotor's body along a straight line, caused by the thrust generated by propulsors.

Signup and view all the flashcards

Rotational Motion in Multirotors

Rotation of the multirotor's body around its axis, caused by the torque generated by propulsors.

Signup and view all the flashcards

Thrust in Multirotor

The force generated by propulsors, pushing the multirotor upwards or in the direction of flight.

Signup and view all the flashcards

Torque in Multirotor

The force that causes the multirotor to rotate around its axis, produced by propulsors.

Signup and view all the flashcards

Drag in Multirotor

The force acting against the multirotor's motion, caused by air resistance.

Signup and view all the flashcards

CW and CCW Rotation in Multirotors

Clockwise (CW) and Counter-Clockwise (CCW) rotation of propulsors to achieve balanced control.

Signup and view all the flashcards

Body Frame and World Frame Relationship

The body frame is attached to the multirotor, while the world frame is fixed. Their relationship defines the multirotor's position and orientation in space.

Signup and view all the flashcards

Early Quadcopter (2006)

The first quadcopter built at FER in 2006, featuring a mechanical gyro for stability.

Signup and view all the flashcards

Mathematical Model of a Multirotor

A set of equations describing the motion of a multirotor based on forces like thrust, torque, and drag.

Signup and view all the flashcards

Simulation Model for Multirotors (Simulink)

A virtual representation of a multirotor in software, used to test and analyze its behavior.

Signup and view all the flashcards

Propeller Thrust Formula

The formula to calculate the thrust generated by a propeller, considering factors like air density, propeller speed, radius, and the local flow velocity.

Signup and view all the flashcards

Induced Velocity

The upward flow of air induced by a propeller's rotation, affecting the overall thrust.

Signup and view all the flashcards

Mechanical Angle

The angle of the propeller blade relative to the plane of rotation, affecting the thrust generated.

Signup and view all the flashcards

Inflow Velocity

The velocity of the air entering the propeller disc, impacting the propeller's performance.

Signup and view all the flashcards

Angle of Attack

The angle between the propeller blade's chord line and the direction of the oncoming airflow, influencing the lift generated.

Signup and view all the flashcards

Propeller Efficiency

The ratio of the useful power produced by the propeller to the power input from the motor, indicating how effectively the propeller utilizes energy.

Signup and view all the flashcards

DC Motor Static Characteristics

A description of how a DC motor's speed and torque vary under different load conditions and input voltage.

Signup and view all the flashcards

Stall Torque

The maximum torque a DC motor can produce before it stalls, indicating its power limit.

Signup and view all the flashcards

No-Load Speed

The speed at which a DC motor rotates without any load, indicating how fast it can turn when unloaded.

Signup and view all the flashcards

Torque Constant

A measure of the torque produced by a DC motor for a given armature current, indicating its efficiency in converting electrical energy into mechanical energy.

Signup and view all the flashcards

Propeller Drag

The resistance force experienced by a rotating propeller due to the air it's moving.

Signup and view all the flashcards

Voltage Drop on Brushes

The decrease in voltage across the brushes of a DC motor due to electrical resistance.

Signup and view all the flashcards

Back Electromagnetic Force

The force generated by a rotating DC motor that opposes the input voltage, affecting the motor's speed and torque.

Signup and view all the flashcards

Motor Power and Torque Relationship

The relationship between the power output by a DC motor and the torque it generates, determined by the motor's speed.

Signup and view all the flashcards

DC Motor Working Point

The operating point of a DC motor, which is the combination of speed and torque at which it operates most efficiently.

Signup and view all the flashcards

Study Notes

Aerial Robotics

  • Study focuses on aerial robotics, specifically unmanned aerial vehicles (UAVs)
  • Course taught by Prof. Stjepan Bogdan, Prof. Matko Orsag, Antun Ivanović, Marko Car, and Lovro Marković
  • Laboratory for Robotics and Intelligent Control Systems, Department of Control and Computer Engineering, University of Zagreb Faculty of Electrical Engineering and Computing

Grading System

  • Two homework assignments (2 x 5 points), minimum 2 points to pass
  • Two lab exercises (2 x 8 points), minimum 4 points to pass (report submissions required)
  • Midterm exam (written): 30 points
  • Final exam (written): 30 points
  • Oral exam: 14 points
  • If a student fails the midterm or final exam, or wants to improve their grade, there are written and oral exams with 60 and 14 points respectively for each.
  • Grading scale:
    • 2: [51-61]
    • 3: [62-77]
    • 4: [78-90]
    • 5 [91-100]

Contents

  • Introduction (history of aerial systems/rotorcrafts)
  • Mathematical Models of UAVs
  • Multirotor Aerodynamics and Actuation
  • Sensors and Control
  • Aerial Manipulator Kinematics
  • Aerial Manipulator Dynamics
  • Mission Planning

History of Aerial Systems

  • 425 BC – Archytas (mechanical bird)
  • 1483 – Leonardo da Vinci (aerial screw)
  • 1843 – George Cayley (aerial coach)
  • 1907 – Paul Cornu (helicopter)
  • 1909 – Igor Sikorsky (unmanned helicopter)
  • 1912 – Boris Yurev (tail rotor)
  • 1916 – Elmer Sperry (gyroscope)
  • Post WWI design: Bothezad (1922), Fa-61 (1936), Sikorsky (1939), Cierva (1923)
  • Modern era (unmanned helicopters): RQ-8A Fire Scout (2002), Schiebel CAMCOPTER (2005)

Mathematical Models of UAVs

  • 6 degrees of freedom (DOF): x, y, z, roll, pitch, yaw
  • UAV as a system: nonlinear, multivariable, coupled, underactuated
  • Complex for control
  • Mathematical model of a blimp: neutral buoyancy, lift = weight, no propulsion
  • Equations of motion (body frame): MV+D(V) v + g(n) = το
  • Mass matrix of blimp's body
  • Matrix D - air friction
  • Gravitational and lift vector assumption
  • Configuration of propulsors- arbitrary number and positions
  • Configuration of propulsors – additional example with 3 propulsors
  • Mathematical model of a helicopter: Fusion 360 Smart BNF, Yamaha R-50
  • Equations of a helicopter motion (rotations): y-z plane (roll), x-z plane (pitch), x-y plane (yaw)
  • Equations of a helicopter motion (translations)
  • Main rotor input, Swash plate input, Tail rotor input
  • Coupling (+linearization): roll, pitch, yaw
  • Small-scale helicopter
  • Simulation example: ellipsoidal blimp, 3 propulsors
  • Simulink model
  • Mathematical model of a multirotor: The first quadcopter at FER (2006)

UAV Applications

  • Military: target and decoy, surveillance and tracking, battle activities, logistics
  • Civilian: Traffic and weather monitoring, firefighting, agriculture, search & rescue, inspection & maintenance, research and development

UAV Control

  • Obstacle Avoidance / Target Tracking
  • Obstacle / Target Identification
  • Obstacle / Target Detection
  • Situation Awareness
  • Mission Planning
  • Mode Selection
  • Mode Transitioning
  • Fault Tolerant Control
  • Flight Control System
  • Emergency Diagnostics
  • UAV Sensors
  • Sensor Fusion
  • Hardware configuration: Sensors (D-GPS, Motion Pak, 3-axis magnetometer, Altitude Sensor), On-Board System (Computer, Flight Control Processor, R-1 Integrated Avionics System) and Ground Station (Hand Held Radio, Control Transmitter, Mission Control Station)
  • Main sensors: IMU (inertial measurement unit), GPS
  • Linear and decoupled control (quadcopter)

Studying That Suits You

Use AI to generate personalized quizzes and flashcards to suit your learning preferences.

Quiz Team

Related Documents

More Like This

Untitled Quiz
6 questions

Untitled Quiz

AdoredHealing avatar
AdoredHealing
Untitled Quiz
37 questions

Untitled Quiz

WellReceivedSquirrel7948 avatar
WellReceivedSquirrel7948
Untitled Quiz
50 questions

Untitled Quiz

JoyousSulfur avatar
JoyousSulfur
Untitled Quiz
48 questions

Untitled Quiz

StraightforwardStatueOfLiberty avatar
StraightforwardStatueOfLiberty
Use Quizgecko on...
Browser
Browser