Polyharmonic spline

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In control theory, a control-Lyapunov function V(x,u) [1]is a generalization of the notion of Lyapunov function V(x) used in stability analysis. The ordinary Lyapunov function is used to test whether a dynamical system is stable (more restrictively, asymptotically stable). That is, whether the system starting in a state x0 in some domain D will remain in D, or for asymptotic stability will eventually return to x=0. The control-Lyapunov function is used to test whether a system is feedback stabilizable, that is whether for any state x there exists a control u(x,t) such that the system can be brought to the zero state by applying the control u.

More formally, suppose we are given a dynamical system

x˙(t)=f(x(t))+g(x(t))u(t),

where the state x(t) and the control u(t) are vectors.

Definition. A control-Lyapunov function is a function V(x,u) that is continuous, positive-definite (that is V(x,u) is positive except at x=0 where it is zero), proper (that is V(x) as |x|), and such that

x0,uV˙(x,u)<0.

The last condition is the key condition; in words it says that for each state x we can find a control u that will reduce the "energy" V. Intuitively, if in each state we can always find a way to reduce the energy, we should eventually be able to bring the energy to zero, that is to bring the system to a stop. This is made rigorous by the following result:

Artstein's theorem. The dynamical system has a differentiable control-Lyapunov function if and only if there exists a regular stabilizing feedback u(x).

It may not be easy to find a control-Lyapunov function for a given system, but if we can find one thanks to some ingenuity and luck, then the feedback stabilization problem simplifies considerably, in fact it reduces to solving a static non-linear programming problem

u*(x)=argminuV(x,u)f(x,u)

for each state x.

The theory and application of control-Lyapunov functions were developed by Z. Artstein and E. D. Sontag in the 1980s and 1990s.

Example

Here is a characteristic example of applying a Lyapunov candidate function to a control problem.

Consider the non-linear system, which is a mass-spring-damper system with spring hardening and position dependent mass described by

m(1+q2)q¨+bq˙+K0q+K1q3=u

Now given the desired state, qd, and actual state, q, with error, e=qdq, define a function r as

r=e˙+αe

A Control-Lyapunov candidate is then

V=12r2

which is positive definite for all q0, q˙0.

Now taking the time derivative of V

V˙=rr˙
V˙=(e˙+αe)(e¨+αe˙)

The goal is to get the time derivative to be

V˙=κV

which is globally exponentially stable if V is globally positive definite (which it is).

Hence we want the rightmost bracket of V˙,

(e¨+αe˙)=(q¨dq¨+αe˙)

to fulfill the requirement

(q¨dq¨+αe˙)=κ2(e˙+αe)

which upon substitution of the dynamics, q¨, gives

(q¨duK0qK1q3bq˙m(1+q2)+αe˙)=κ2(e˙+αe)

Solving for u yields the control law

u=m(1+q2)(q¨d+αe˙+κ2r)+K0q+K1q3+bq˙

with κ and α, both greater than zero, as tunable parameters

This control law will guarantee global exponential stability since upon substitution into the time derivative yields, as expected

V˙=κV

which is a linear first order differential equation which has solution

V=V(0)eκt

And hence the error and error rate, remembering that V=12(e˙+αe)2, exponentially decay to zero.

If you wish to tune a particular response from this, it is necessary to substitute back into the solution we derived for V and solve for e. This is left as an exercise for the reader but the first few steps at the solution are:

rr˙=κ2r2
r˙=κ2r
r=r(0)eκ2t
e˙+αe=(e˙(0)+αe(0))eκ2t

which can then be solved using any linear differential equation methods.

Notes

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References

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See also

  1. Freeman (46)