Symmetry-preserving filter – Wikipedia

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In mathematics, Symmetry-preserving observers,[1][2] also known as invariant filters, are estimation techniques whose structure and design take advantage of the natural symmetries (or invariances) of the considered nonlinear model. As such, the main benefit is an expected much larger domain of convergence than standard filtering methods, e.g. Extended Kalman Filter (EKF) or Unscented Kalman Filter (UKF).

Motivation[edit]

Most physical systems possess natural symmetries (or invariance), i.e. there exist transformations (e.g. rotations, translations, scalings) that leave the system unchanged. From mathematical and engineering viewpoints, it makes sense that a filter well-designed for the system being considered should preserve the same invariance properties.

Definition[edit]

Consider

G{displaystyle G}

a Lie group, and
(local) transformation groups

φg,ψg,ρg{displaystyle varphi _{g},psi _{g},rho _{g}}

, where

gG{displaystyle gin G}

.

The nonlinear system

is said to be invariant if it is left unchanged by the action of

φg,ψg,ρg{displaystyle varphi _{g},psi _{g},rho _{g}}

, i.e.

where

(X,U,Y)=(φg(x),ψg(u),ρg(y)){displaystyle (X,U,Y)=(varphi _{g}(x),psi _{g}(u),rho _{g}(y))}

.

The system

x^˙=F(x^,u,y){displaystyle {dot {hat {x}}}=F({hat {x}},u,y)}

is then an invariant filter if

General equation and main result[edit]

It has been proved [1] that every invariant observer reads

where

Given the system and the associated transformation group being considered, there exists a constructive method to determine

E(x^,u,y),W(x^),I(x^,u){displaystyle E({hat {x}},u,y),W({hat {x}}),I({hat {x}},u)}

, based on the moving frame method.

To analyze the error convergence, an invariant state error

η(x^,x){displaystyle eta ({hat {x}},x)}

is defined, which is different from the standard output error

x^x{displaystyle {hat {x}}-x}

, since the standard output error usually does not preserve the symmetries of the system. One of the main benefits of symmetry-preserving filters is that the error system is “autonomous“, but for the free known invariant vector

I(x^,u){displaystyle I({hat {x}},u)}

, i.e.

η˙=Υ(η,I(x^,u)){displaystyle {dot {eta }}=Upsilon {bigl (}eta ,I({hat {x}},u){bigr )}}

. This important property allows the estimator to have a very large domain of convergence, and to be easy to tune.[3][4]

To choose the gain matrix

L(I,E){displaystyle L(I,E)}

, there are two possibilities:

  • a deterministic approach, that leads to the construction of truly nonlinear symmetry-preserving filters (similar to Luenberger-like observers)
  • a stochastic approach, that leads to Invariant Extended Kalman Filters (similar to Kalman-like observers).

Applications[edit]

There has been numerous applications that use such invariant observers to estimate the state of the considered system. The application areas include

References[edit]

  1. ^ a b c S. Bonnabel, Ph. Martin, and P. Rouchon, “Symmetry-preserving observers,”
    IEEE Transactions on Automatic and Control, vol. 53, no. 11, pp. 2514–2526, 2008.
  2. ^ S. Bonnabel, Ph. Martin and E. Salaün, “Invariant Extended Kalman Filter: theory and application to a velocity-aided attitude estimation problem”, 48th IEEE Conference on Decision and Control, pp. 1297-1304, 2009.
  3. ^ a b Ph. Martin and E. Salaün, “An invariant observer for Earth-velocity-aided attitude heading reference
    systems”, 17th IFAC World Congress, pp. 9857-9864, 2008.
  4. ^ a b Ph. Martin and E. Salaün, “Design and implementation of a low-cost observer-based Attitude and Heading Reference System”, Control Engineering Practice, 2010.