Difference between revisions of "State Feedback"

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(Created page with "{{Chapter |Chapter number=7 |Previous chapter=Linear Systems |Next chapter=Output Feedback |Chapter summary=This chapter describes how feedback can be used to shape the local...")
 
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{{Chapter
 
{{Chapter
 
|Chapter number=7
 
|Chapter number=7
 +
|Short name=statefbk
 
|Previous chapter=Linear Systems
 
|Previous chapter=Linear Systems
 
|Next chapter=Output Feedback
 
|Next chapter=Output Feedback
 +
|First edition URL=https://www.cds.caltech.edu/~murray/amwiki/index.php?title=State_Feedback#Additional_Exercises
 
|Chapter summary=This chapter describes how feedback can be used to shape the local behavior of a system. The concept of reachability is introduced and used to investigate how to "design" the dynamics of a system through placement of its eigenvalues. In particular, it will be shown that under certain conditions it is possible to assign the system eigenvalues to arbitrary values by appropriate feedback of the system state.
 
|Chapter summary=This chapter describes how feedback can be used to shape the local behavior of a system. The concept of reachability is introduced and used to investigate how to "design" the dynamics of a system through placement of its eigenvalues. In particular, it will be shown that under certain conditions it is possible to assign the system eigenvalues to arbitrary values by appropriate feedback of the system state.
|Chapter contents=# Reachability
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|Chapter contents=# Observability
# Stabilization by State Feedback
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#* Definition of Observability
#* Example: Vectored thrust aircraft
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#* Testing for Observability
# State Feedback Design Issues
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#* Observable Canonical Form
# Integral Action
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# State Estimation
 +
#* The Observer
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#* Computing the Observer Gain
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# Control Using Estimated State
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#* Kalman's Decomposition of a Linear System
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# Kalman Filtering
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#* Discrete-Time Systems
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#* Continuous-Time Systems
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#* Linear Quadratic Gaussian Control (LQG)
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# State Space Controller Design
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#* Two Degree-of-Freedom Controller Architecture
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#* Feedforward Design and Trajectory Generation
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#* Disturbance Modeling and State Augmentation
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#* Feedback Design and Gain Scheduling
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#* Nonlinear Estimation
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#* Computer Implementation
 
# Further Reading
 
# Further Reading
 
:: Exercises
 
:: Exercises
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\end{aligned}
 
\end{aligned}
 
</math></center>
 
</math></center>
is said to be ''reachable'' if we can find an input <math>u(t)</math> defined on the interval <amsmath>[0, T]</amsmath> that can steer the system from a given final point <amsmath>x(0) = x_0</amsmath> to a desired final point <math>x(T) = x_f</math>.
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is said to be ''reachable'' if we can find an input <math>u(t)</math> defined on the interval <math>[0, T]</math> that can steer the system from a given final point <math>x(0) = x_0</math> to a desired final point <math>x(T) = x_f</math>.
 
</p></li>
 
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     x_e = -(A-BK)^{-1} B k_\text{f} r \qquad y_e = C x_e.
 
     x_e = -(A-BK)^{-1} B k_\text{f} r \qquad y_e = C x_e.
 
</math></center>
 
</math></center>
Choosing <amsmath>k_r</amsmath> as
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Choosing <math>k_\text{f}</math> as
 
<center><math>
 
<center><math>
 
   k_r = {-1}/\left(C (A-BK)^{-1} B\right).
 
   k_r = {-1}/\left(C (A-BK)^{-1} B\right).
 
</math></center>
 
</math></center>
gives <math>y_e = r</amsmath>.</p></li>
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gives <math>y_e = r</math>.</p></li>
  
 
<li><p>If a system is reachable, then there exists a feedback law of the form
 
<li><p>If a system is reachable, then there exists a feedback law of the form
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<li><p>''Integral feedback'' can be used to provide zero steady state error instead of careful calibration of the gain <math>k_\text{f}</math>.  An integral feedback controller has the form
 
<li><p>''Integral feedback'' can be used to provide zero steady state error instead of careful calibration of the gain <math>k_\text{f}</math>.  An integral feedback controller has the form
<center><amsmath>
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<center><math>
 
  u = -K (x - x_\text{e}) - k_\text{i} z + k_\text{f} r,
 
  u = -K (x - x_\text{e}) - k_\text{i} z + k_\text{f} r,
</amsmath></center>
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</math></center>
 
where
 
where
 
<center><math>
 
<center><math>

Revision as of 21:33, 28 August 2021

Prev: Linear Systems Chapter 7 - State Feedback Next: Output Feedback
Statefbk-firstpage.png

This chapter describes how feedback can be used to shape the local behavior of a system. The concept of reachability is introduced and used to investigate how to "design" the dynamics of a system through placement of its eigenvalues. In particular, it will be shown that under certain conditions it is possible to assign the system eigenvalues to arbitrary values by appropriate feedback of the system state.

Chapter Summary

This chapter describes how state feedback can be used to design the (closed loop) dynamics of the system:

  1. A linear system with dynamics

    is said to be reachable if we can find an input defined on the interval that can steer the system from a given final point to a desired final point .

  2. The reachability matrix for a linear system is given by

    A linear system is reachable if and only if the reachability matrix is invertible (assuming a single intput/single output system). Systems that are not reachable have states that are constrained to have a fixed relationship with each other.

  3. A linear system of the form

    is said to be in reachable canonical form. A system in this form is always reachable and has a characteristic polynomial given by

    A reachable linear system can be transformed into reachable canonical form through the use of a coordinate transformation .

  4. A state feedback law has the form

    where is the reference value for the output. The closed loop dynamics for the system are given by

    The stability of the system is determined by the stability of the matrix . The equilibrium point and steady state output (assuming the systems is stable) are given by

    Choosing as

    gives .

  5. If a system is reachable, then there exists a feedback law of the form

    the gives a closed loop system with an arbitrary characteristic polynomial. Hence the eigenvalues of a reachable linear system can be placed arbitrarily through the use of an appropriate feedback control law.

  6. Integral feedback can be used to provide zero steady state error instead of careful calibration of the gain . An integral feedback controller has the form

    where

    is the integral error. The gains , and can be found by designing a stabilizing state feedback for the system dynamics augmented by the integrator dynamics.

  7. A linear quadratic regulator minimizes the cost function

    The solution to the LQR problem is given by a linear control law of the form

    where is a positive definite, symmetric matrix that satisfies the equation

    This equation is called the algebraic Riccati equation and can be solved numerically.


Teaching Materials

None available

Additional Exercises

None available

Frequently Asked Questions

None available

Errata

None reported

Python Code

The following Python scripts are available for producing figures that appear in this chapter.

See the software page for more information on how to run these scripts.

Additional Information