Introduction Chapter 1 - PowerPoint PPT Presentation

1 / 23
About This Presentation
Title:

Introduction Chapter 1

Description:

Is the study of the motion of systems with the corresponding analysis of forces ... angular momentum and the developed electromagnetic torque as function of time. ... – PowerPoint PPT presentation

Number of Views:49
Avg rating:3.0/5.0
Slides: 24
Provided by: ahma1
Category:

less

Transcript and Presenter's Notes

Title: Introduction Chapter 1


1
Introduction(Chapter 1)
BEE3163 ELECTROMECHANICAL SYSTEMS
2
Mechatronics and Emerging Trends in Engineering
  • Mechatronics is a system-level approach to
    designing electromechanical systems that merges
    mechanical, electrical, control system, and
    embedded software design.
  • It represents an industry-wide effort to improve
    the design process by integrating the best
    available development practices and technologies
    to streamline design, prototyping, and
    deployment.

3
  • Why Study Mechatronics
  • If you design industrial machinery, equipment,
    vehicles, or other devices with moving parts and
    electronically controlled actuators, mechatronics
    technology may help you lower development costs,
    reduce risk, and produce higher-quality
    products.Benefits of Mechatronics
  • Higher profitability through faster, lower-risk,
    lower-cost development
  • Increased efficiency due to better communication,
    collaboration, and integration
  • Greater innovation through increased design
    automation across engineering domains

4
Mechatronics and Emerging Trends in Engineering
  • Electromechanical System Integrate
    electromechanical motion devices (actuator and
    sensors), transducers (analog and digital), power
    electronics and converters, controllers (analog
    and digital), data equisition system and etc

5
Mechatronics and Emerging Trends in Engineering
  • Electromechanical motion devices studied using
    electromagnetics and mechanics
  • Electromechanical energy conversion devices
    convert electrical energy to mechanical energy
    and mechanical energy to electrical energy
  • Actuator control by power converters (eg to
    regulate the angular velocity of electric motor)
    and control algorithm should be designed to
    control electromechanical systems
  • Transducer is a device, usually electrical,
    electronic, electro-mechanical, electromagnetic,
    photonic, or photovoltaic that converts one type
    of energy to another for various purposes
    including measurement or information transfer
    (for example, pressure sensors)
  • These control laws implemented using analog and
    digital controllers, and PC DSP hardware and
    microcontrollers

6
Mechatronics and Emerging Trends in Engineering
  • Mechatronics is a multi-disiplinary concepts,
    integrates electrical, mechanical, and software
    engineering
  • Example mechatronics concept motion control
    problem in aircraft. The aircraft is controlled
    by flight control surface
  • Direct drive servo system are used to actuate
    these control surface
  • This system fly-by-wire flight servo system
    actuated by stepper motor

7
Fly-by-wire
  • Mechanical and hydraulic flight control systems
    are heavy and require careful routing of flight
    control cables through the aircraft using systems
    of pulley, cranks, wires and, with
    hydraulically-assisted controls, hydraulic pipes.
  • Both systems often require redundant backup,
    which further increases weight

8
Fly-by-Wire
  • The words Fly-by-Wire imply only an
    electrically-signalled control system.
  • The term is generally used, however, in the sense
    of computer-configured controls.
  • This is where, between the operator and the final
    control actuator or surface, a computer system is
    interposed.
  • This modifies the inputs of the pilot (or
    operator for non-aircraft systems) in accordance
    with software programmes.
  • Mechatronics and Emerging Trends in Engineering

9
Mechanical
  • The flight control systems uses a collection of
    mechanical parts such as rods, cables, pulleys
    and sometimes chains to transmit the forces of
    the cockpit controls to the control surfaces.
  • Since an increase in control surface area in
    bigger and faster aircraft leads to a large
    increase in the forces needed to move them,
    complicated mechanical arrangements are used to
    extract maximum mechanical advantage in order to
    make the forces required bearable to the pilots.

10
Hydraulic
  • A hydraulic flight control systems has 2 parts
  • The mechanical circuit
  • The mechanical circuit links the cockpit controls
    with the hydraulic circuits. Like the mechanical
    flight control systems, it is made of rods,
    cables, pulleys, and sometimes chains.
  • The hydraulic circuit
  • The hydraulic circuit has hydraulic pumps, pipes,
    valves and actuators.
  • The actuators are powered by the hydraulic
    pressure generated by the pumps in the hydraulic
    circuit.
  • The actuators convert hydraulic pressure into
    control surface movements. The servo valves
    control the movement of the actuators.

11
Mechatronics and Emerging Trends in Engineering
  • Mechtronics concept is applied to approach and
    solve dynamics and control problems. Example
    high level closed loop flight control system,
    robotics system
  • Mechatronics emerges as a most general concept
    that provide a systematic and unified conceptual
    framework in analysis and optimization,
    prototyping and design, and control and
    deployment of a system

12
Mechatronics and Emerging Trends in Engineering
  • Modern electromehanical system rely increasingly
    on digital controllers (microprocessor and DSP)
  • Block diagram of typical digitally controlled
    system
  • The design specification imosed on
    electromechanical system are given in the system
    domain. The commonly used performance criteria to
    be attained are
  • Stability with the desired stability margins in
    the full operating envelope
  • Robustness to parameters variations and
    structural changes
  • Tracking and disturbance attenuation
  • Dynamic and steady state accuracy
  • Specification imposed on the states and outputs
    transient response

13
Unit step response of a 2nd order underdamped
system
14
BASIC FOUNDATION
  • Electromechanical system must be studied using
    the fundamental laws and basic principles of
    mechanics and electromagnetics
  • Mechanics
  • Is the study of the motion of systems with the
    corresponding analysis of forces that cause
    motion is of interest
  • Newtons second law of motion states that the net
    vector acting on an object of mass m is related
    to its acceleration vector

15
BASIC FOUNDATION
  • In the Cartesian (XYZ) coordinate system
  • represent the magnitude and direction of
    the net force acting on the object. is
    not a force
  • A body at equilibrium that is the object is at
    rest or moving with constant speed

16
BASIC FOUNDATION
  • Newtons second law of motion in terms of linear
    which is found as

For rotational motion, the net torque and angular
acceleration must be used. The torque vector
17
BASIC FOUNDATION
  • The rotational analog of Newtons second law for
    a rigid body

18
BASIC FOUNDATION
  • The angular momentum of the system is expressed by

For the rigid body rotating around the axis of
symmetry
19
BASIC FOUNDATION
  • Example 1
  • An electric motor has the equivalent moment of
    inertia J0.06kgm2. The motor starts from the
    stall and the angular velocity of the motor is
  • Find the angular momentum and the developed
    electromagnetic torque as function of time. The
    load and friction torque are zero.

20
BASIC FOUNDATION
  • From newtonian mechanics the applied net force
    plays a central role in quantitatively describing
    the motion.
  • Total energy of the system

For translational motion of a body to an ideal
spring
21
BASIC FOUNDATION
For rotational spring
Kinetic energy of translation and rotation
The moment of inertia is depends on how the mass
is distributed with respect to the axis, and J is
different for different axes of rotation
22
BASIC FOUNDATION
Assuming the body is rigid, and the moment of
inertia, J is constant
The total work is given by
The change if the kinetic energy
23
BASIC FOUNDATION
Power is defined by
In analog which is applied for translational
motion, Power
Example 1.6 An electric motor drives a load
and the electromagnetic torque developed by the
motor is 0.2 N.m (Te0.2N.m). The motor starts
from stall and has the equivalent moment of
inertia 0.01 kg.m2 (J 0.01 kg.m2 ). Calculate
the work and kinetic energy at t15s
Write a Comment
User Comments (0)
About PowerShow.com