Digital Control Lab
1. MAGNETIC LEVITATION
MagLev apparatus dramatically demonstrates closed loop levitation of permanent
and ferromagnetic elements. The apparatus includes laser feedback and high flux
magnetics to affect large displacements and provide visually stimulating tracking
and regulation demonstrations.
The system is quickly set up in the open loop
stable and unstable (repulsive and attractive fields) configurations. By adding
a second magnet and driving both actuators, MIMO control is studied.
The inherent
magnetic field nonlinearities may be inverted via provided real-time algorithms for
linear control study or the full system dynamics may be examined.
Disturbances may
be introduced via the second drive coil for demonstrating system regulation in SISO
operation. An optional turn table accessory provides graphic demonstration of induced
field levitation - the principal used in high speed bullet trains.
2. RECTILINEAR PLANT
This classical system appears commonly in dynamics and controls
text books and serves as a benchmark for control method evaluation. This system
provides vivid demonstrations of elementary topics such as rigid body PID control,
lead/lag compensators, phase and gain margin, trajectory tracking, and regulation -
as well as advanced high order collocated and noncollocated system control. The
apparatus also clearly demonstrates salient properties of flexible systems such as
mode shapes, natural frequencies, and characteristic transient and frequency
responses. An optional secondary drive may be positioned at any output (mass carriage)
to create a MIMO plant and provide for the study of disturbance rejection. Study of
this system provides the first steps in understanding parameter estimation and system
identification occuring in large plants.
3. TWIN ROTOR MULTIPLE INPUT MULTIPLE OUTPUT (TRMS) MODEL
The TRMS workshop serves as a model of a helicopter. However some significant
simplifications are made. First is the fact that TRMS is attached to a tower
and second that the helicopter position and velocity is controlled through the
rotor velocity vasriation. In the real helicopter the rotor velocity is not constant
and the propulsion is varied through the rotor blades angle modification.
Nevertheless the most important dynamic characteristics present in a helicopter
are captured in the TRMS model. like in a real helicopter there is a significant
cross coupling between two rotors. If we activate the vertical position rotor the
helicopter will also turn in the horizontal plane.
With two inputs (the voltages supplied to the rotors) and outputs (vertical and
horizontal angles and angular velocities) the TRMS is an excellent MIMO plant for
getting started with a helicopter!
4. PIC MICROCONTROLLER
PIC is a family of modified Harvard architecture microcontrollers made by
Microchip Technology, derived from the PIC 1650 originally developed by
General Instrument's Microelectronics Division. The name PIC initially
referred to "Peripheral Interface Controller". PIC's are popular with both
industrial developers and hobbyists alike due to their low cost, large user
base, extensive collection of application notes, availability of low cost or
free development tools, and serial programming capability.
These PICs are programmed using MATRIX MULTIMEDIAs E-blocks circuit board.
E-blocks are small circuit boards each of which contains a block electronics
that one would typically find in an electronic or embedded system. There are
many circuit boards in the range; from simple LED boards to more complex boards
like device programmers, Bluetooth, TCP/IP and many more. These blocks can be
snapped together to form a wide variety of systems that can be used for learning
electronics and for the rapid prototyping of complex electronic system.
5. GYROSCOPE
ECP's four axis Control Moment Gyroscope is a dynamically
rich system that provides superb demonstrations of multi-DOF
rigid body control. Elementary experiments that graphically show
the phenomenon of gyroscopic torque and its use in precision high
authority control are readily performed. More advanced topics range
from MIMO linear control to fully general nonlinear control with
singularity avoidance. Thus the system yields demonstrations that
are intriguing to the layman and post-doctorate alike! In addition,
the plant may be used to emulate the control of satellite attitude.
The apparatus includes low friction slip rings at all gimbals for
unlimited range of motion, and precision encoders for feedback of all
position and velocity states. A host of safety features such as fail-safe brakes,
inertial rate sensing switches, and real-time watch-dog monitoring provide for
safe operation of the apparatus.
6. INVERTED PENDULUM
This unique ECP design vividly demonstrates the need for and effectiveness
of closed loop control. It is not the conventional rod-on-cart inverted pendulum,
but rather, it steers a horizontal balancing rod in the presence of gravity
to control the vertical pendulum rod. The plant has both right half plane poles
and zeros as well as kinematic and gravitationally coupled nonlinearities. By
adjusting mass properties, these roots may be varied to make the control problem
range from being relatively simple to theoretically impossible! The system
includes removable and adjustable moment arm counterweights on the vertical
and horizontal rods for quick adjustment of the plant dynamics. It features
linear and rotary ball bearings at the joints for low friction and consistent
dynamic properties.
