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You can choose an avatar and change the default style by going to "Profile" → "Personality" or "Display".Dear all, I am trying to calculate (T1/S0)roam, (S0/S1)roam and (T1/S1)roam for roaming reaction of nitrobenzene, but no these structures through geometric optimization all the time, I would like to consult how I should modify input to make it work properly and obtain the same structures with previous paper [DOI: 10.1039/d0cp02077j].
Through a thorough exploration of the system PEHs, performing a series of CASSCF MECP optimizations imposing restrictions in the C1N7 bond distance and re-evaluating the energies at the CASPT2 level, a new T1/S0 STC region featuring a detachment of the nitro group, hereafter (T1/S0)roam, has been characterized. The structure is also a S0/S1 conical intersection (CI) and T1/S1 STC, since the three states (S0, S1, and T1) are degenerate (Table 1). In the (T1/S0)roam region the CASSCF(16,13) S0 wave-function is mainly described by a single closed-shell configuration state function, while both S1 and T1
are mostly described by a single one-electron promotion from what can be recognized as the b2 orbital of the NO2 molecule to the s* orbital associated with the original CN bond in nitrobenzene (Fig. S10, ESI†).42 The SOC between S0 and T1 at the (T1/S0)roam geometry is 48 cm-1
Here is my input:
&GATEWAY
coord=14
nitrobenzene
C -0.20342400 -0.09288600 0.09800890
C 0.00652330 -1.25722000 -0.58106000
C 0.18176000 -1.19926000 -1.98502000
C 0.15133900 0.05781950 -2.62266000
C -0.15272200 1.20163000 -1.91517000
C -0.29733800 1.17933000 -0.52176600
N -0.26723700 0.27407100 2.36788000
O -0.27435900 -0.95750100 2.52781000
O 0.86164500 0.48634000 1.87991000
H 0.03363930 -2.22232000 -0.08691810
H 0.38452400 -2.08796000 -2.55013000
H 0.30355300 0.10772200 -3.69072000
H -0.23875900 2.16609000 -2.43146000
H -0.48914600 2.05020000 0.05310090
basis = ANO-L-MB
Group = NoSym
Constraints
a = Ediff
Values
a = 0.000
End of constraints
>>> EXPORT MOLCAS_MAXITER=500
>>> Do while
&SEWARD
>>> If ( Iter = 1 ) <<<
&SCF
>>> EndIf <<<
&RASSCF
Nactel = 10
Ras2 = 10
Spin = 1
Inactive = 53
Charge= 0
CiRoot=2 2 1
Rlxroot=1
&ALASKA
PNEW
>>COPY $WorkDir/$Project.RunFile $WorkDir/RUNFILE2
&RASSCF
Nactel = 10
Ras2 = 10
Spin = 3
Inactive = 53
Charge= 0
CiRoot=2 2 1
Rlxroot=1
&ALASKA
PNEW
&SLAPAF
>>> EndDo
the structure after optimization:
O -3.73180600 -1.06267661 -0.44598944
O -2.37478070 0.05481752 -1.95480864
N -2.98163186 -1.25972063 -1.50477837
C -0.59666908 1.45860004 0.89783004
C 0.67972248 1.59332618 0.16332013
C 1.42114823 0.45906175 -0.29747015
H 2.41927461 0.58504925 -0.86568208
C 0.87507268 -0.88441502 -0.04675520
C -0.37122725 -1.11193088 0.66248621
C -1.06696227 0.09614574 1.13255599
H -1.18498535 2.39317781 1.24288642
H 1.10956338 2.52896929 -0.02266064
H 1.37172408 -1.57533274 -0.87311513
H -0.83803357 -2.10765946 0.66402040
However, the structure obtained in the previous paper as follows:
C -0.20342400 -0.09288600 0.09800890
C 0.00652330 -1.25722000 -0.58106000
C 0.18176000 -1.19926000 -1.98502000
C 0.15133900 0.05781950 -2.62266000
C -0.15272200 1.20163000 -1.91517000
C -0.29733800 1.17933000 -0.52176600
N -0.26723700 0.27407100 2.36788000
O -0.27435900 -0.95750100 2.52781000
O 0.86164500 0.48634000 1.87991000
H 0.03363930 -2.22232000 -0.08691810
H 0.38452400 -2.08796000 -2.55013000
H 0.30355300 0.10772200 -3.69072000
H -0.23875900 2.16609000 -2.43146000
H -0.48914600 2.05020000 0.05310090
So, I hope can solve how to revise the input file to obtain the structure in the previous paper. Thank you for your help.
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