A Carathéodory-π solution is a generalized solution to an ordinary differential equation. The concept is due to I. Michael Ross and named in honor of Constantin Carathéodory.[1] Its practicality was demonstrated in 2008 by Ross et al.[2] in a laboratory implementation of the concept. The concept is most useful for implementing feedback controls, particularly those generated by an application of Ross' pseudospectral optimal control theory.[3]
A Carathéodory-π solution addresses the fundamental problem of defining a solution to a differential equation,
when g(x,t) is not differentiable with respect to x. Such problems arise quite naturally[4] in defining the meaning of a solution to a controlled differential equation,
when the control, u, is given by a feedback law,
where the function k(x,t) may be non-smooth with respect to x. Non-smooth feedback controls arise quite often in the study of optimal feedback controls and have been the subject of extensive study going back to the 1960s.[5]
An ordinary differential equation,
is equivalent to a controlled differential equation,
with feedback control, u = g ( x , t ) {\displaystyle u=g(x,t)} . Then, given an initial value problem, Ross partitions the time interval [ 0 , ∞ ) {\displaystyle [0,\infty )} to a grid, π = { t i } i ≥ 0 {\displaystyle \pi =\{t_{i}\}_{i\geq 0}} with t i → ∞ as i → ∞ {\displaystyle t_{i}\to \infty {\text{ as }}i\to \infty } . From t 0 {\displaystyle t_{0}} to t 1 {\displaystyle t_{1}} , generate a control trajectory,
to the controlled differential equation,
A Carathéodory solution exists for the above equation because t ↦ u {\displaystyle t\mapsto u} has discontinuities at most in t, the independent variable. At t = t 1 {\displaystyle t=t_{1}} , set x 1 = x ( t 1 ) {\displaystyle x_{1}=x(t_{1})} and restart the system with u ( t ) = g ( x 1 , t ) {\displaystyle u(t)=g(x_{1},t)} ,
Continuing in this manner, the Carathéodory segments are stitched together to form a Carathéodory-π solution.
A Carathéodory-π solution can be applied towards the practical stabilization of a control system.[6][7] It has been used to stabilize an inverted pendulum,[6] control and optimize the motion of robots,[7][8] slew and control the NPSAT1 spacecraft[3] and produce guidance commands for low-thrust space missions.[2]