Opened 20 months ago
Closed 18 months ago
#2957 closed enhancement (done)
Implement symbolic regression problem instances from "A multilevel block building algorithm for fast modeling generalized separable systems"
Reported by: | gkronber | Owned by: | gkronber |
---|---|---|---|
Priority: | medium | Milestone: | HeuristicLab 3.3.16 |
Component: | Problems.Instances | Version: | trunk |
Keywords: | Cc: |
Description (last modified by gkronber)
See: https://arxiv.org/abs/1706.02281
This paper uses data from physical formulas as benchmark problems. The formulas are complex (complex non-separable terms, several variables and variable references, etc.). It also describes comparisons with experiments using the "Eureka" software (convenient for further papers!).
Interesting formulas are listed in Equation 2.1, 2.2 and 2.4, ranges for variable values are in the appendix. Ranges for values and "readable" formulas are given in the appendix.
Change History (11)
comment:1 Changed 20 months ago by gkronber
- Owner set to gkronber
- Status changed from new to accepted
comment:2 Changed 20 months ago by gkronber
- Description modified (diff)
comment:3 Changed 20 months ago by gkronber
comment:4 Changed 19 months ago by gkronber
r16394: reviewed implementation and made some adjustments.
The "maximum lift of whole aircraft" is only described in the arXiv version of the paper but has been removed in the peer-reviewed version for ESWA. There seems to be an error in the pre-print (x5 and x6 stand for only one variable in the original formula and the ranges for valid values are missing).
I decided to keep the problem and assumed a rather large range to make the problem more interesting for benchmarking purposes. All differences to the published version of the problem instances are described.
comment:5 Changed 19 months ago by gkronber
There were two significant changes made in r16394:
- for the lift coefficicent, I changed x1*(x2 - 2) + ... to C_L = C_La (a + 2) + ... because the paper states that a0 is set to -2° in C_La (a - a0)
- for the flow psi problem, I changed x1*x2*x5*(1 - x4²/x5²) + ... to V_inf r sin(th) (1 - R²/r²) + .... So it is now necessary to identify the function sin(th) as a factor.
comment:6 Changed 19 months ago by gkronber
- Status changed from accepted to readytorelease
- Version set to trunk
comment:7 Changed 19 months ago by lkammere
r16431: Fixed visibility of regression instance providers for physics benchmark problems.
comment:8 Changed 19 months ago by mkommend
- Status changed from readytorelease to reviewing
comment:9 Changed 18 months ago by gkronber
- Status changed from reviewing to readytorelease
Reviewed r16431.
comment:10 Changed 18 months ago by gkronber
comment:11 Changed 18 months ago by gkronber
- Resolution set to done
- Status changed from readytorelease to closed
r16264: initial import of physics problems implemented by lkammere