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Controllability
Encyclopedia
Controllability is an important property of a control system
, and the controllability property plays a crucial role in many control problems, such as stabilization of unstable systems
by feedback, or optimal control.
Controllability and observability
are dual
aspects of the same problem.
Roughly, the concept of controllability denotes the ability to move a system around in its entire configuration space using only certain admissible manipulations. The exact definition varies slightly within the framework or the type of models applied.
The following are examples of variations of controllability notions which have been introduced in the systems and control literature:
of a system, which is a collection of the system's variables values, completely describes the system at any given time. In particular, no information on the past of a system will help in predicting the future, if the states at the present time are known.
Complete state controllability (or simply controllability if no other context is given) describes the ability of an external input to move the internal state of a system from any initial state to any other final state in a finite time interval.
linear
time-variant system
There exists a control
from state
at time
to state
at time
if and only if
is in the column space
of
where
is the state-transition matrix
.
In fact, if
is a solution to
then a control given by
would make the desired transfer.
Note that the matrix
defined as above has the following properties:
where
The
controllability matrix is given by
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-39.gif)
The system is controllable if the controllability matrix has full rank
(i.e.
).
) the state equation is
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-42.gif)
Where
is an
matrix and
is a
matrix (i.e.
is
inputs collected in a
vector. The test for controllability is that the
matrix
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-51.gif)
has full row rank
(i.e.,
). That is, if the system is controllable,
will have
columns that are linearly independent; if
columns of
are linearly independent, each of the
states is reachable giving the system proper inputs through the variable
.
and
(i.e. only one control input). Thus,
and
are
vectors. If
has rank 2 (full rank), and so
and
are linearly independent and span the entire plane. If the rank is 1, then
and
are collinear
and do not span the plane.
Assume that the initial state is zero.
At time
: ![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-70.gif)
At time
: ![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-72.gif)
At time
all of the reachable states are on the line formed by the vector
.
At time
all of the reachable states are linear combinations of
and
.
If the system is controllable then these two vectors can span the entire plane and can be done so for time
.
The assumption made that the initial state is zero is merely for convenience.
Clearly if all states can be reached from the origin then any state can be reached from another state (merely a shift in coordinates).
This example holds for all positive
, but the case of
is easier to visualize.
to the previous example system.
You are sitting in your car on an infinite, flat plane and facing north.
The goal is to reach any point in the plane by driving a distance in a straight line, come to a full stop, turn, and driving another distance, again, in a straight line.
If your car has no steering then you can only drive straight, which means you can only drive on a line (in this case the north-south line since you started facing north).
The lack of steering case would be analogous to when the rank of
is 1 (the two distances you drove are on the same line).
Now, if your car did have steering then you could easily drive to any point in the plane and this would be the analogous case to when the rank of
is 2.
If you change this example to
then the analogy would be flying in space to reach any position in 3D space (ignoring the orientation
of the aircraft
).
You are allowed to:
Although the 3-dimensional case is harder to visualize, the concept of controllability is still analogous.
is locally accessible about
if the accessibility distribution
spans
space, when
equals the rank of
and R is given by:
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-90.gif)
Here,
is the repeated Lie bracket
operation defined by
The controllability matrix for linear systems in the previous section can in fact be derived from this equation.
For a linear continuous-time system, like the example above, described by matrices
,
,
, and
, the
output controllability matrix![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-98.gif)
must have full row rank (i.e. rank
) if and only if the system is output controllable.
), models considered do not directly define an input–output structure. In this framework systems are described by admissible trajectories of a collection of variables, some of which might be interpreted as inputs or outputs.
A system is then defined to be controllable in this setting, if any past part of a behavior (trajectory of the external veriables) can be concatenated with any future trajectory of the behavior in such a way that the concatenation is contained in the behavior, i.e. is part of the admissible system behavior.
Control system
A control system is a device, or set of devices to manage, command, direct or regulate the behavior of other devices or system.There are two common classes of control systems, with many variations and combinations: logic or sequential controls, and feedback or linear controls...
, and the controllability property plays a crucial role in many control problems, such as stabilization of unstable systems
BIBO stability
In electrical engineering, specifically signal processing and control theory, BIBO stability is a form of stability for linear signals and systems that take inputs. BIBO stands for Bounded-Input Bounded-Output...
by feedback, or optimal control.
Controllability and observability
Observability
Observability, in control theory, is a measure for how well internal states of a system can be inferred by knowledge of its external outputs. The observability and controllability of a system are mathematical duals. The concept of observability was introduced by American-Hungarian scientist Rudolf E...
are dual
Duality (mathematics)
In mathematics, a duality, generally speaking, translates concepts, theorems or mathematical structures into other concepts, theorems or structures, in a one-to-one fashion, often by means of an involution operation: if the dual of A is B, then the dual of B is A. As involutions sometimes have...
aspects of the same problem.
Roughly, the concept of controllability denotes the ability to move a system around in its entire configuration space using only certain admissible manipulations. The exact definition varies slightly within the framework or the type of models applied.
The following are examples of variations of controllability notions which have been introduced in the systems and control literature:
- State controllability
- Output controllability
- Controllability in the behavioural framework
State controllability
The stateState space (controls)
In control engineering, a state space representation is a mathematical model of a physical system as a set of input, output and state variables related by first-order differential equations...
of a system, which is a collection of the system's variables values, completely describes the system at any given time. In particular, no information on the past of a system will help in predicting the future, if the states at the present time are known.
Complete state controllability (or simply controllability if no other context is given) describes the ability of an external input to move the internal state of a system from any initial state to any other final state in a finite time interval.
Continuous linear systems
Consider the continuousContinuous function
In mathematics, a continuous function is a function for which, intuitively, "small" changes in the input result in "small" changes in the output. Otherwise, a function is said to be "discontinuous". A continuous function with a continuous inverse function is called "bicontinuous".Continuity of...
linear
Linear
In mathematics, a linear map or function f is a function which satisfies the following two properties:* Additivity : f = f + f...
time-variant system
Time-variant system
A time-variant system is a system that is not time invariant . Roughly speaking, characteristics of its output depend explicitly upon time.- Overview :...
There exists a control
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-3.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-4.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-5.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-6.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-7.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-8.gif)
Column space
In linear algebra, the column space of a matrix is the set of all possible linear combinations of its column vectors. The column space of an m × n matrix is a subspace of m-dimensional Euclidean space...
of
where
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-10.gif)
State-transition matrix
In control theory, the state-transition matrix is a matrix whose product with the state vector x at an initial time t_0 gives x at a later time t. The state-transition matrix can be used to obtain the general solution of linear dynamical systems...
.
In fact, if
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-11.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-12.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-13.gif)
Note that the matrix
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-14.gif)
-
is symmetric
-
is positive semidefinite for
-
satisfies the linear matrix differential equation
Matrix differential equationA differential equation is a mathematical equation for an unknown function of one or several variables that relates the values of the function itself and of its derivatives of various orders...
-
-
-
satisfies the equation
-
-
-
Continuous linear time-invariant (LTI) systems
Consider the continuous linear time-invariant systemTime-invariant system
A time-invariant system is one whose output does not depend explicitly on time.This property can be satisfied if the transfer function of the system is not a function of time except expressed by the input and output....
where
-
is the
"state vector",
-
is the
"output vector",
-
is the
"input (or control) vector",
-
is the
"state matrix",
-
is the
"input matrix",
-
is the
"output matrix",
-
is the
"feedthrough (or feedforward) matrix".
The
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-38.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-39.gif)
The system is controllable if the controllability matrix has full rank
Rank (linear algebra)
The column rank of a matrix A is the maximum number of linearly independent column vectors of A. The row rank of a matrix A is the maximum number of linearly independent row vectors of A...
(i.e.
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-40.gif)
Discrete linear time-invariant (LTI) systems
For a discrete-time linear state-space system (i.e. time variable![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-41.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-42.gif)
Where
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-43.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-44.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-45.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-46.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-47.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-48.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-49.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-50.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-51.gif)
has full row rank
Rank (linear algebra)
The column rank of a matrix A is the maximum number of linearly independent column vectors of A. The row rank of a matrix A is the maximum number of linearly independent row vectors of A...
(i.e.,
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-52.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-53.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-54.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-55.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-56.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-57.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-58.gif)
Example
For example, consider the case when![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-59.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-60.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-61.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-62.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-63.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-64.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-65.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-66.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-67.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-68.gif)
Line (geometry)
The notion of line or straight line was introduced by the ancient mathematicians to represent straight objects with negligible width and depth. Lines are an idealization of such objects...
and do not span the plane.
Assume that the initial state is zero.
At time
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-69.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-70.gif)
At time
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-71.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-72.gif)
At time
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-73.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-74.gif)
At time
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-75.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-76.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-77.gif)
If the system is controllable then these two vectors can span the entire plane and can be done so for time
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-78.gif)
The assumption made that the initial state is zero is merely for convenience.
Clearly if all states can be reached from the origin then any state can be reached from another state (merely a shift in coordinates).
This example holds for all positive
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-79.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-80.gif)
Analogy for example of n = 2
Consider an analogyCar analogy
The car analogy is a common resort exploited by engineering textbooks to ease the understanding of some abstract concepts found within it.-Uses of car analogies:...
to the previous example system.
You are sitting in your car on an infinite, flat plane and facing north.
The goal is to reach any point in the plane by driving a distance in a straight line, come to a full stop, turn, and driving another distance, again, in a straight line.
If your car has no steering then you can only drive straight, which means you can only drive on a line (in this case the north-south line since you started facing north).
The lack of steering case would be analogous to when the rank of
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-81.gif)
Now, if your car did have steering then you could easily drive to any point in the plane and this would be the analogous case to when the rank of
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-82.gif)
If you change this example to
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-83.gif)
Orientation (rigid body)
In geometry the orientation, angular position, or attitude of an object such as a line, plane or rigid body is part of the description of how it is placed in the space it is in....
of the aircraft
Aircraft
An aircraft is a vehicle that is able to fly by gaining support from the air, or, in general, the atmosphere of a planet. An aircraft counters the force of gravity by using either static lift or by using the dynamic lift of an airfoil, or in a few cases the downward thrust from jet engines.Although...
).
You are allowed to:
- fly in a straight line
- turn left or right by any amount (Yaw)
- direct the plane upwards or downwards by any amount (Pitch)
Although the 3-dimensional case is harder to visualize, the concept of controllability is still analogous.
Nonlinear systems
Nonlinear systems in the control-affine formis locally accessible about
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-85.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-86.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-87.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-88.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-89.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-90.gif)
Here,
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-91.gif)
Lie bracket of vector fields
In the mathematical field of differential topology, the Lie bracket of vector fields, Jacobi–Lie bracket, or commutator of vector fields is a bilinear differential operator which assigns, to any two vector fields X and Y on a smooth manifold M, a third vector field denoted [X, Y]...
operation defined by
The controllability matrix for linear systems in the previous section can in fact be derived from this equation.
Output controllability
Output controllability is the related notion for the output of the system; the output controllability describes the ability of an external input to move the output from any initial condition to any final condition in a finite time interval. It is not necessary that there is any relationship between state controllability and output controllability. In particular:- A controllable system is not necessarily output controllable. For example, if matrix D = 0 and matrix C does not have full row rank, then some positions of the output are masked by the limiting structure of the output matrix. Moreover, even though the system can be moved to any state in finite time, there may be some outputs that are inaccessible by all states. A trivial numerical example uses D=0 and a C matrix with at least one row of zeros; thus, the system is not able to produce a non-zero output along that dimension.
- An output controllable system is not necessarily controllable. For example, if the dimension of the state space is greater than the dimension of the output, then there will be a set of possible state configurations for each individual output. That is, the system can have significant zero dynamics, which are trajectories of the system that are not observable from the output. Consequently, being able to drive an output to a particular position in finite time says nothing about the state configuration of the system.
For a linear continuous-time system, like the example above, described by matrices
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-93.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-94.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-95.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-96.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-97.gif)
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-98.gif)
must have full row rank (i.e. rank
![](http://image.absoluteastronomy.com/images/formulas/7/0/1700997-99.gif)
Controllability in the behavioural framework
In the so-called behavioral system theoretic approach due to Willems (see people in systems and controlPeople in systems and control
This is an alphabetical list of people who have made significant contributions in the fields of system analysis and control theory.-Active researchers:-Historical figures in systems and control:...
), models considered do not directly define an input–output structure. In this framework systems are described by admissible trajectories of a collection of variables, some of which might be interpreted as inputs or outputs.
A system is then defined to be controllable in this setting, if any past part of a behavior (trajectory of the external veriables) can be concatenated with any future trajectory of the behavior in such a way that the concatenation is contained in the behavior, i.e. is part of the admissible system behavior.