Execution Chart

We display below the execution chart for this examination (boot time has been removed).

Trace from the execution

Formatting '/data/fkordon/mcc2023-input.r001-oct2-167813588300169.qcow2', fmt=qcow2 cluster_size=65536 extended_l2=off compression_type=zlib size=4294967296 backing_file=/data/fkordon/mcc2023-input.qcow2 backing_fmt=qcow2 lazy_refcounts=off refcount_bits=16
Waiting for the VM to be ready (probing ssh)
.......................
=====================================================================
Generated by BenchKit 2-5348
Executing tool marcie
Input is AirplaneLD-COL-0010, examination is CTLCardinality
Time confinement is 3600 seconds
Memory confinement is 16384 MBytes
Number of cores is 1
Run identifier is r001-oct2-167813588300169
=====================================================================

--------------------
preparation of the directory to be used:
/home/mcc/execution
total 444K
-rw-r--r-- 1 mcc users 7.7K Feb 26 11:10 CTLCardinality.txt
-rw-r--r-- 1 mcc users 74K Feb 26 11:10 CTLCardinality.xml
-rw-r--r-- 1 mcc users 5.6K Feb 26 11:08 CTLFireability.txt
-rw-r--r-- 1 mcc users 49K Feb 26 11:08 CTLFireability.xml
-rw-r--r-- 1 mcc users 4.2K Jan 29 11:40 GenericPropertiesDefinition.xml
-rw-r--r-- 1 mcc users 6.5K Jan 29 11:40 GenericPropertiesVerdict.xml
-rw-r--r-- 1 mcc users 3.9K Feb 25 15:30 LTLCardinality.txt
-rw-r--r-- 1 mcc users 24K Feb 25 15:30 LTLCardinality.xml
-rw-r--r-- 1 mcc users 2.4K Feb 25 15:30 LTLFireability.txt
-rw-r--r-- 1 mcc users 18K Feb 25 15:30 LTLFireability.xml
-rw-r--r-- 1 mcc users 11K Feb 26 11:13 ReachabilityCardinality.txt
-rw-r--r-- 1 mcc users 93K Feb 26 11:13 ReachabilityCardinality.xml
-rw-r--r-- 1 mcc users 6.8K Feb 26 11:12 ReachabilityFireability.txt
-rw-r--r-- 1 mcc users 54K Feb 26 11:12 ReachabilityFireability.xml
-rw-r--r-- 1 mcc users 1.8K Feb 25 15:30 UpperBounds.txt
-rw-r--r-- 1 mcc users 3.8K Feb 25 15:30 UpperBounds.xml
-rw-r--r-- 1 mcc users 5 Mar 5 18:22 equiv_pt
-rw-r--r-- 1 mcc users 5 Mar 5 18:22 instance
-rw-r--r-- 1 mcc users 5 Mar 5 18:22 iscolored
-rw-r--r-- 1 mcc users 40K Mar 5 18:22 model.pnml

--------------------
content from stdout:

=== Data for post analysis generated by BenchKit (invocation template)

The expected result is a vector of booleans
BOOL_VECTOR

here is the order used to build the result vector(from text file)
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-00
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-01
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-02
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-03
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-04
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-05
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-06
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-07
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-08
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-09
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-10
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-11
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-12
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-13
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-14
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-15

=== Now, execution of the tool begins

BK_START 1678387863449

bash -c /home/mcc/BenchKit/BenchKit_head.sh 2> STDERR ; echo ; echo -n "BK_STOP " ; date -u +%s%3N
Invoking MCC driver with
BK_TOOL=marcie
BK_EXAMINATION=CTLCardinality
BK_BIN_PATH=/home/mcc/BenchKit/bin/
BK_TIME_CONFINEMENT=3600
BK_INPUT=AirplaneLD-COL-0010
Not applying reductions.
Model is COL
CTLCardinality COL
timeout --kill-after=10s --signal=SIGINT 1m for testing only

Marcie built on Linux at 2019-11-18.
A model checker for Generalized Stochastic Petri nets

authors: Alex Tovchigrechko (IDD package and CTL model checking)

Martin Schwarick (Symbolic numerical analysis and CSL model checking)

Christian Rohr (Simulative and approximative numerical model checking)

marcie@informatik.tu-cottbus.de

called as: /home/mcc/BenchKit/bin//../marcie/bin/marcie --net-file=model.pnml --mcc-file=CTLCardinality.xml --memory=6 --mcc-mode

parse successfull
net created successfully

Unfolding complete |P|=89|T|=88|A|=333
Time for unfolding: 0m 1.353sec

Net: AirplaneLD_COL_0010
(NrP: 89 NrTr: 88 NrArc: 333)

parse formulas
formulas created successfully
place and transition orderings generation:0m 0.001sec

net check time: 0m 0.000sec

init dd package: 0m 3.105sec


RS generation: 0m 0.035sec


-> reachability set: #nodes 1372 (1.4e+03) #states 43,463 (4)



starting MCC model checker
--------------------------

checking: EF [AG [AF [87<=P4_dot]]]
normalized: E [true U ~ [E [true U EG [~ [87<=P4_dot]]]]]

abstracting: (87<=P4_dot)
states: 0

EG iterations: 0
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-CTLCardinality-11 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.012sec

checking: EF [60<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)]
normalized: E [true U 60<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)]

abstracting: (60<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0))
states: 0
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-CTLCardinality-00 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.022sec

checking: [AF [56<=stp1_dot] & AF [~ [[63<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0) & AF [~ [AF [sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=71]]]]]]]
normalized: [~ [EG [[63<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0) & ~ [EG [~ [EG [~ [sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=71]]]]]]]] & ~ [EG [~ [56<=stp1_dot]]]]

abstracting: (56<=stp1_dot)
states: 0

EG iterations: 0
abstracting: (sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=71)
states: 43,463 (4)
.
EG iterations: 1

EG iterations: 0
abstracting: (63<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0))
states: 0
.
EG iterations: 1
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-CTLCardinality-04 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.055sec

checking: A [P2_dot<=stp3_dot U [EG [[EG [AF [stp5_dot<=2]] & stp2_dot<=92]] | AF [AG [[33<=P3_dot & AF [P3_dot<=17]]]]]]
normalized: [~ [EG [~ [[~ [EG [E [true U ~ [[33<=P3_dot & ~ [EG [~ [P3_dot<=17]]]]]]]] | EG [[stp2_dot<=92 & EG [~ [EG [~ [stp5_dot<=2]]]]]]]]]] & ~ [E [~ [[~ [EG [E [true U ~ [[33<=P3_dot & ~ [EG [~ [P3_dot<=17]]]]]]]] | EG [[stp2_dot<=92 & EG [~ [EG [~ [stp5_dot<=2]]]]]]]] U [~ [P2_dot<=stp3_dot] & ~ [[~ [EG [E [true U ~ [[33<=P3_dot & ~ [EG [~ [P3_dot<=17]]]]]]]] | EG [[stp2_dot<=92 & EG [~ [EG [~ [stp5_dot<=2]]]]]]]]]]]]

abstracting: (stp5_dot<=2)
states: 43,463 (4)
.
EG iterations: 1

EG iterations: 0
abstracting: (stp2_dot<=92)
states: 43,463 (4)

EG iterations: 0
abstracting: (P3_dot<=17)
states: 43,463 (4)
.
EG iterations: 1
abstracting: (33<=P3_dot)
states: 0

EG iterations: 0
abstracting: (P2_dot<=stp3_dot)
states: 36,203 (4)
abstracting: (stp5_dot<=2)
states: 43,463 (4)
.
EG iterations: 1

EG iterations: 0
abstracting: (stp2_dot<=92)
states: 43,463 (4)

EG iterations: 0
abstracting: (P3_dot<=17)
states: 43,463 (4)
.
EG iterations: 1
abstracting: (33<=P3_dot)
states: 0

EG iterations: 0
abstracting: (stp5_dot<=2)
states: 43,463 (4)
.
EG iterations: 1

EG iterations: 0
abstracting: (stp2_dot<=92)
states: 43,463 (4)

EG iterations: 0
abstracting: (P3_dot<=17)
states: 43,463 (4)
.
EG iterations: 1
abstracting: (33<=P3_dot)
states: 0

EG iterations: 0
.
EG iterations: 1
-> the formula is TRUE

FORMULA AirplaneLD-COL-0010-CTLCardinality-01 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.004sec

checking: EX [[EG [~ [53<=stp5_dot]] & AG [[stp3_dot<=stp1_dot | AF [AX [P2_dot<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)]]]]]]
normalized: EX [[~ [E [true U ~ [[~ [EG [EX [~ [P2_dot<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)]]]] | stp3_dot<=stp1_dot]]]] & EG [~ [53<=stp5_dot]]]]

abstracting: (53<=stp5_dot)
states: 0

EG iterations: 0
abstracting: (stp3_dot<=stp1_dot)
states: 41,769 (4)
abstracting: (P2_dot<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0))
states: 43,463 (4)
..
EG iterations: 1
.-> the formula is TRUE

FORMULA AirplaneLD-COL-0010-CTLCardinality-12 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.024sec

checking: E [AF [[EX [A [P3_dot<=19 U P2_dot<=P2_dot]] | AX [76<=stp1_dot]]] U AG [AX [EG [sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)<=P1_dot]]]]
normalized: E [~ [EG [~ [[~ [EX [~ [76<=stp1_dot]]] | EX [[~ [EG [~ [P2_dot<=P2_dot]]] & ~ [E [~ [P2_dot<=P2_dot] U [~ [P3_dot<=19] & ~ [P2_dot<=P2_dot]]]]]]]]]] U ~ [E [true U EX [~ [EG [sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)<=P1_dot]]]]]]

abstracting: (sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)<=P1_dot)
states: 33,165 (4)
...........
EG iterations: 11
.abstracting: (P2_dot<=P2_dot)
states: 43,463 (4)
abstracting: (P3_dot<=19)
states: 43,463 (4)
abstracting: (P2_dot<=P2_dot)
states: 43,463 (4)
abstracting: (P2_dot<=P2_dot)
states: 43,463 (4)
.
EG iterations: 1
.abstracting: (76<=stp1_dot)
states: 0
..
EG iterations: 1
-> the formula is TRUE

FORMULA AirplaneLD-COL-0010-CTLCardinality-06 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.371sec

checking: [EG [[EF [[E [91<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0) U stp3_dot<=stp4_dot] & [39<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0) & ~ [stp5_dot<=19]]]] | ~ [P2_dot<=stp4_dot]]] & EG [stp3_dot<=99]]
normalized: [EG [[E [true U [E [91<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0) U stp3_dot<=stp4_dot] & [39<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0) & ~ [stp5_dot<=19]]]] | ~ [P2_dot<=stp4_dot]]] & EG [stp3_dot<=99]]

abstracting: (stp3_dot<=99)
states: 43,463 (4)

EG iterations: 0
abstracting: (P2_dot<=stp4_dot)
states: 36,533 (4)
abstracting: (stp5_dot<=19)
states: 43,463 (4)
abstracting: (39<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0))
states: 0
abstracting: (stp3_dot<=stp4_dot)
states: 41,593 (4)
abstracting: (91<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0))
states: 0
.....
EG iterations: 5
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-CTLCardinality-10 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.064sec

checking: AG [AG [E [[100<=P3_dot | [[stp1_dot<=stp2_dot & P3_dot<=46] | AG [P4_dot<=stp5_dot]]] U ~ [EG [32<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)]]]]]
normalized: ~ [E [true U E [true U ~ [E [[100<=P3_dot | [~ [E [true U ~ [P4_dot<=stp5_dot]]] | [stp1_dot<=stp2_dot & P3_dot<=46]]] U ~ [EG [32<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)]]]]]]]

abstracting: (32<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1))
states: 0
.
EG iterations: 1
abstracting: (P3_dot<=46)
states: 43,463 (4)
abstracting: (stp1_dot<=stp2_dot)
states: 38,381 (4)
abstracting: (P4_dot<=stp5_dot)
states: 43,353 (4)
abstracting: (100<=P3_dot)
states: 0
-> the formula is TRUE

FORMULA AirplaneLD-COL-0010-CTLCardinality-15 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.032sec

checking: EX [AG [[A [P3_dot<=P6_dot U 53<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)] | ~ [EG [[sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)<=59 | sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)<=35]]]]]]
normalized: EX [~ [E [true U ~ [[[~ [EG [~ [53<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)]]] & ~ [E [~ [53<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)] U [~ [P3_dot<=P6_dot] & ~ [53<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)]]]]] | ~ [EG [[sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)<=59 | sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)<=35]]]]]]]]

abstracting: (sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)<=35)
states: 43,463 (4)
abstracting: (sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)<=59)
states: 43,463 (4)

EG iterations: 0
abstracting: (53<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1))
states: 0
abstracting: (P3_dot<=P6_dot)
states: 40,922 (4)
abstracting: (53<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1))
states: 0
abstracting: (53<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1))
states: 0

EG iterations: 0
.-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-CTLCardinality-05 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 2.316sec

checking: ~ [[EF [[[[P4_dot<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0) & P4_dot<=stp2_dot] & ~ [E [stp1_dot<=71 U 42<=stp3_dot]]] & sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=3]] | [EG [EG [EG [26<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)]]] & EF [E [EX [sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)] U [AX [P5_dot<=19] & 53<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)]]]]]]
normalized: ~ [[[EG [EG [EG [26<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)]]] & E [true U E [EX [sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)] U [53<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1) & ~ [EX [~ [P5_dot<=19]]]]]]] | E [true U [sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=3 & [~ [E [stp1_dot<=71 U 42<=stp3_dot]] & [P4_dot<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0) & P4_dot<=stp2_dot]]]]]]

abstracting: (P4_dot<=stp2_dot)
states: 43,342 (4)
abstracting: (P4_dot<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0))
states: 43,342 (4)
abstracting: (42<=stp3_dot)
states: 0
abstracting: (stp1_dot<=71)
states: 43,463 (4)
abstracting: (sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=3)
states: 43,463 (4)
abstracting: (P5_dot<=19)
states: 43,463 (4)
.abstracting: (53<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1))
states: 0
abstracting: (sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0))
states: 38,381 (4)
.abstracting: (26<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0))
states: 0
.
EG iterations: 1
.
EG iterations: 1
.
EG iterations: 1
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-CTLCardinality-02 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 2.403sec

checking: AX [~ [EF [EF [EG [sum(TheAltitude_Altitude9, TheAltitude_Altitude8, TheAltitude_Altitude7, TheAltitude_Altitude6, TheAltitude_Altitude5, TheAltitude_Altitude4, TheAltitude_Altitude3, TheAltitude_Altitude20, TheAltitude_Altitude2, TheAltitude_Altitude19, TheAltitude_Altitude18, TheAltitude_Altitude17, TheAltitude_Altitude16, TheAltitude_Altitude15, TheAltitude_Altitude14, TheAltitude_Altitude13, TheAltitude_Altitude12, TheAltitude_Altitude11, TheAltitude_Altitude10, TheAltitude_Altitude1)<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)]]]]]
normalized: ~ [EX [E [true U E [true U EG [sum(TheAltitude_Altitude9, TheAltitude_Altitude8, TheAltitude_Altitude7, TheAltitude_Altitude6, TheAltitude_Altitude5, TheAltitude_Altitude4, TheAltitude_Altitude3, TheAltitude_Altitude20, TheAltitude_Altitude2, TheAltitude_Altitude19, TheAltitude_Altitude18, TheAltitude_Altitude17, TheAltitude_Altitude16, TheAltitude_Altitude15, TheAltitude_Altitude14, TheAltitude_Altitude13, TheAltitude_Altitude12, TheAltitude_Altitude11, TheAltitude_Altitude10, TheAltitude_Altitude1)<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)]]]]]

abstracting: (sum(TheAltitude_Altitude9, TheAltitude_Altitude8, TheAltitude_Altitude7, TheAltitude_Altitude6, TheAltitude_Altitude5, TheAltitude_Altitude4, TheAltitude_Altitude3, TheAltitude_Altitude20, TheAltitude_Altitude2, TheAltitude_Altitude19, TheAltitude_Altitude18, TheAltitude_Altitude17, TheAltitude_Altitude16, TheAltitude_Altitude15, TheAltitude_Altitude14, TheAltitude_Altitude13, TheAltitude_Altitude12, TheAltitude_Altitude11, TheAltitude_Altitude10, TheAltitude_Altitude1)<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1))
MC time: 9m59.014sec

checking: [~ [EF [~ [A [[[stp1_dot<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1) & sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)] | 72<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)] U EF [P4_dot<=sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)]]]]] | [EF [[[EX [[sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)<=51 & 12<=stp4_dot]] & E [~ [33<=P2_dot] U [50<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0) & 50<=P3_dot]]] & P4_dot<=53]] | EG [22<=P2_dot]]]
normalized: [[E [true U [P4_dot<=53 & [EX [[sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)<=51 & 12<=stp4_dot]] & E [~ [33<=P2_dot] U [50<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0) & 50<=P3_dot]]]]] | EG [22<=P2_dot]] | ~ [E [true U ~ [[~ [E [~ [E [true U P4_dot<=sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)]] U [~ [E [true U P4_dot<=sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)]] & ~ [[72<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0) | [stp1_dot<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1) & sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)]]]]]] & ~ [EG [~ [E [true U P4_dot<=sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)]]]]]]]]]

abstracting: (P4_dot<=sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1))
states: 43,452 (4)
.
EG iterations: 1
abstracting: (sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0))
states: 43,463 (4)
abstracting: (stp1_dot<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1))
states: 43,463 (4)
abstracting: (72<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0))
states: 0
abstracting: (P4_dot<=sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1))
states: 43,452 (4)
abstracting: (P4_dot<=sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1))
states: 43,452 (4)
abstracting: (22<=P2_dot)
states: 0
.
EG iterations: 1
abstracting: (50<=P3_dot)
states: 0
abstracting: (50<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0))
states: 0
abstracting: (33<=P2_dot)
states: 0
abstracting: (12<=stp4_dot)
states: 0
abstracting: (sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)<=51)
states: 43,463 (4)
.abstracting: (P4_dot<=53)
states: 43,463 (4)
-> the formula is TRUE

FORMULA AirplaneLD-COL-0010-CTLCardinality-13 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.149sec

checking: ~ [EF [E [[[EF [P6_dot<=39] | [sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)<=P1_dot & ~ [stp3_dot<=90]]] | EX [EF [stp3_dot<=41]]] U E [EX [32<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)] U [~ [sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)<=28] & E [P3_dot<=55 U P3_dot<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)]]]]]]
normalized: ~ [E [true U E [[[[sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)<=P1_dot & ~ [stp3_dot<=90]] | E [true U P6_dot<=39]] | EX [E [true U stp3_dot<=41]]] U E [EX [32<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)] U [~ [sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)<=28] & E [P3_dot<=55 U P3_dot<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)]]]]]]

abstracting: (P3_dot<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1))
states: 43,463 (4)
abstracting: (P3_dot<=55)
states: 43,463 (4)
abstracting: (sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)<=28)
states: 43,463 (4)
abstracting: (32<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1))
states: 0
.abstracting: (stp3_dot<=41)
states: 43,463 (4)
.abstracting: (P6_dot<=39)
states: 43,463 (4)
abstracting: (stp3_dot<=90)
states: 43,463 (4)
abstracting: (sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)<=P1_dot)
states: 0
-> the formula is TRUE

FORMULA AirplaneLD-COL-0010-CTLCardinality-08 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 4.685sec

checking: E [[AG [[EF [[sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)<=P1_dot | 52<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)]] & E [[79<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0) | stp5_dot<=P6_dot] U stp3_dot<=92]]] | ~ [[~ [EG [P3_dot<=stp5_dot]] & [~ [P5_dot<=51] & ~ [[sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)<=58 & sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)<=94]]]]]] U A [~ [P5_dot<=41] U [[AG [[stp1_dot<=14 | sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=54]] & [sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=19 & [stp2_dot<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0) | ~ [stp4_dot<=P3_dot]]]] & AX [[14<=P4_dot & [39<=stp1_dot & sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)]]]]]]
normalized: E [[~ [[[~ [[sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)<=58 & sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)<=94]] & ~ [P5_dot<=51]] & ~ [EG [P3_dot<=stp5_dot]]]] | ~ [E [true U ~ [[E [[79<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0) | stp5_dot<=P6_dot] U stp3_dot<=92] & E [true U [sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)<=P1_dot | 52<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)]]]]]]] U [~ [E [~ [[~ [EX [~ [[14<=P4_dot & [39<=stp1_dot & sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)]]]]] & [~ [E [true U ~ [[stp1_dot<=14 | sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=54]]]] & [sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=19 & [stp2_dot<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0) | ~ [stp4_dot<=P3_dot]]]]]] U [P5_dot<=41 & ~ [[~ [EX [~ [[14<=P4_dot & [39<=stp1_dot & sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)]]]]] & [~ [E [true U ~ [[stp1_dot<=14 | sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=54]]]] & [sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=19 & [stp2_dot<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0) | ~ [stp4_dot<=P3_dot]]]]]]]]] & ~ [EG [~ [[~ [EX [~ [[14<=P4_dot & [39<=stp1_dot & sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)]]]]] & [~ [E [true U ~ [[stp1_dot<=14 | sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=54]]]] & [sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=19 & [stp2_dot<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0) | ~ [stp4_dot<=P3_dot]]]]]]]]]]

abstracting: (stp4_dot<=P3_dot)
states: 39,745 (4)
abstracting: (stp2_dot<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0))
states: 43,463 (4)
abstracting: (sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=19)
states: 43,463 (4)
abstracting: (sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=54)
states: 43,463 (4)
abstracting: (stp1_dot<=14)
states: 43,463 (4)
abstracting: (sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0))
states: 0
abstracting: (39<=stp1_dot)
states: 0
abstracting: (14<=P4_dot)
states: 0
............
EG iterations: 11
abstracting: (stp4_dot<=P3_dot)
states: 39,745 (4)
abstracting: (stp2_dot<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0))
states: 43,463 (4)
abstracting: (sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=19)
states: 43,463 (4)
abstracting: (sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=54)
states: 43,463 (4)
abstracting: (stp1_dot<=14)
states: 43,463 (4)
abstracting: (sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0))
states: 0
abstracting: (39<=stp1_dot)
states: 0
abstracting: (14<=P4_dot)
states: 0
.abstracting: (P5_dot<=41)
states: 43,463 (4)
abstracting: (stp4_dot<=P3_dot)
states: 39,745 (4)
abstracting: (stp2_dot<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0))
states: 43,463 (4)
abstracting: (sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=19)
states: 43,463 (4)
abstracting: (sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=54)
states: 43,463 (4)
abstracting: (stp1_dot<=14)
states: 43,463 (4)
abstracting: (sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0))
states: 0
abstracting: (39<=stp1_dot)
states: 0
abstracting: (14<=P4_dot)
states: 0
.abstracting: (52<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0))
states: 0
abstracting: (sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)<=P1_dot)
states: 0
abstracting: (stp3_dot<=92)
states: 43,463 (4)
abstracting: (stp5_dot<=P6_dot)
states: 40,448 (4)
abstracting: (79<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0))
states: 0
abstracting: (P3_dot<=stp5_dot)
states: 41,153 (4)
.....
EG iterations: 5
abstracting: (P5_dot<=51)
states: 43,463 (4)
abstracting: (sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)<=94)
states: 43,463 (4)
abstracting: (sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)<=58)
states: 43,463 (4)
-> the formula is TRUE

FORMULA AirplaneLD-COL-0010-CTLCardinality-03 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 9.166sec

checking: A [E [~ [76<=stp5_dot] U ~ [[AF [[sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)<=89 | stp3_dot<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)]] | [[A [42<=stp1_dot U 81<=P4_dot] & ~ [27<=stp4_dot]] | [EX [P3_dot<=55] & [sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)<=13 | stp1_dot<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)]]]]]] U EG [[[stp2_dot<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1) & ~ [[~ [sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)<=25] | ~ [sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)<=62]]]] & EF [EX [sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)]]]]]
normalized: [~ [EG [~ [EG [[[stp2_dot<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1) & ~ [[~ [sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)<=62] | ~ [sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)<=25]]]] & E [true U EX [sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)]]]]]]] & ~ [E [~ [EG [[[stp2_dot<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1) & ~ [[~ [sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)<=62] | ~ [sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)<=25]]]] & E [true U EX [sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)]]]]] U [~ [E [~ [76<=stp5_dot] U ~ [[~ [EG [~ [[sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)<=89 | stp3_dot<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)]]]] | [[EX [P3_dot<=55] & [sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)<=13 | stp1_dot<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)]] | [[~ [E [~ [81<=P4_dot] U [~ [81<=P4_dot] & ~ [42<=stp1_dot]]]] & ~ [EG [~ [81<=P4_dot]]]] & ~ [27<=stp4_dot]]]]]]] & ~ [EG [[[stp2_dot<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1) & ~ [[~ [sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)<=62] | ~ [sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)<=25]]]] & E [true U EX [sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)]]]]]]]]]

abstracting: (sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0))
states: 13,323 (4)
.abstracting: (sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)<=25)
states: 43,463 (4)
abstracting: (sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)<=62)
states: 43,463 (4)
abstracting: (stp2_dot<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1))
states: 42,308 (4)
..........
EG iterations: 10
abstracting: (27<=stp4_dot)
states: 0
abstracting: (81<=P4_dot)
states: 0

EG iterations: 0
abstracting: (42<=stp1_dot)
states: 0
abstracting: (81<=P4_dot)
states: 0
abstracting: (81<=P4_dot)
states: 0
abstracting: (stp1_dot<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0))
states: 35,840 (4)
abstracting: (sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)<=13)
states: 43,463 (4)
abstracting: (P3_dot<=55)
states: 43,463 (4)
.abstracting: (stp3_dot<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1))
states: 43,463 (4)
abstracting: (sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)<=89)
states: 43,463 (4)
.
EG iterations: 1
abstracting: (76<=stp5_dot)
states: 0
abstracting: (sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0))
states: 13,323 (4)
.abstracting: (sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)<=25)
states: 43,463 (4)
abstracting: (sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)<=62)
states: 43,463 (4)
abstracting: (stp2_dot<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1))
states: 42,308 (4)
..........
EG iterations: 10
abstracting: (sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0))
states: 13,323 (4)
.abstracting: (sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)<=25)
states: 43,463 (4)
abstracting: (sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)<=62)
states: 43,463 (4)
abstracting: (stp2_dot<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1))
states: 42,308 (4)
..........
EG iterations: 10

EG iterations: 0
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-CTLCardinality-07 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 4.793sec

checking: [[~ [A [[[stp4_dot<=51 | sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)<=64] & 98<=stp1_dot] U 34<=P6_dot]] & EF [[[[[EG [stp1_dot<=43] & [P4_dot<=31 | 8<=stp4_dot]] & ~ [AF [stp2_dot<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)]]] & EG [AG [P6_dot<=P5_dot]]] | ~ [[E [P6_dot<=38 U sum(TheAltitude_Altitude9, TheAltitude_Altitude8, TheAltitude_Altitude7, TheAltitude_Altitude6, TheAltitude_Altitude5, TheAltitude_Altitude4, TheAltitude_Altitude3, TheAltitude_Altitude20, TheAltitude_Altitude2, TheAltitude_Altitude19, TheAltitude_Altitude18, TheAltitude_Altitude17, TheAltitude_Altitude16, TheAltitude_Altitude15, TheAltitude_Altitude14, TheAltitude_Altitude13, TheAltitude_Altitude12, TheAltitude_Altitude11, TheAltitude_Altitude10, TheAltitude_Altitude1)<=sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)] | EX [sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=P1_dot]]]]]] & [E [[P3_dot<=P1_dot | AG [AG [19<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)]]] U stp2_dot<=stp2_dot] & AG [[[sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)<=44 | [[AX [9<=P4_dot] & ~ [71<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)]] & 58<=stp5_dot]] | A [[E [53<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1) U 8<=stp4_dot] | [sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)<=P4_dot & stp2_dot<=77]] U 5<=stp4_dot]]]]]
normalized: [[E [[P3_dot<=P1_dot | ~ [E [true U E [true U ~ [19<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)]]]]] U stp2_dot<=stp2_dot] & ~ [E [true U ~ [[[sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)<=44 | [58<=stp5_dot & [~ [EX [~ [9<=P4_dot]]] & ~ [71<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)]]]] | [~ [E [~ [5<=stp4_dot] U [~ [5<=stp4_dot] & ~ [[E [53<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1) U 8<=stp4_dot] | [sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)<=P4_dot & stp2_dot<=77]]]]]] & ~ [EG [~ [5<=stp4_dot]]]]]]]]] & [E [true U [~ [[EX [sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=P1_dot] | E [P6_dot<=38 U sum(TheAltitude_Altitude9, TheAltitude_Altitude8, TheAltitude_Altitude7, TheAltitude_Altitude6, TheAltitude_Altitude5, TheAltitude_Altitude4, TheAltitude_Altitude3, TheAltitude_Altitude20, TheAltitude_Altitude2, TheAltitude_Altitude19, TheAltitude_Altitude18, TheAltitude_Altitude17, TheAltitude_Altitude16, TheAltitude_Altitude15, TheAltitude_Altitude14, TheAltitude_Altitude13, TheAltitude_Altitude12, TheAltitude_Altitude11, TheAltitude_Altitude10, TheAltitude_Altitude1)<=sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)]]] | [EG [~ [E [true U ~ [P6_dot<=P5_dot]]]] & [EG [~ [stp2_dot<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)]] & [[P4_dot<=31 | 8<=stp4_dot] & EG [stp1_dot<=43]]]]]] & ~ [[~ [EG [~ [34<=P6_dot]]] & ~ [E [~ [34<=P6_dot] U [~ [[98<=stp1_dot & [stp4_dot<=51 | sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)<=64]]] & ~ [34<=P6_dot]]]]]]]]

abstracting: (34<=P6_dot)
states: 0
abstracting: (sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)<=64)
states: 43,463 (4)
abstracting: (stp4_dot<=51)
states: 43,463 (4)
abstracting: (98<=stp1_dot)
states: 0
abstracting: (34<=P6_dot)
states: 0
abstracting: (34<=P6_dot)
states: 0

EG iterations: 0
abstracting: (stp1_dot<=43)
states: 43,463 (4)

EG iterations: 0
abstracting: (8<=stp4_dot)
states: 0
abstracting: (P4_dot<=31)
states: 43,463 (4)
abstracting: (stp2_dot<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1))
states: 43,463 (4)
.
EG iterations: 1
abstracting: (P6_dot<=P5_dot)
states: 33,165 (4)
.
EG iterations: 1
abstracting: (sum(TheAltitude_Altitude9, TheAltitude_Altitude8, TheAltitude_Altitude7, TheAltitude_Altitude6, TheAltitude_Altitude5, TheAltitude_Altitude4, TheAltitude_Altitude3, TheAltitude_Altitude20, TheAltitude_Altitude2, TheAltitude_Altitude19, TheAltitude_Altitude18, TheAltitude_Altitude17, TheAltitude_Altitude16, TheAltitude_Altitude15, TheAltitude_Altitude14, TheAltitude_Altitude13, TheAltitude_Altitude12, TheAltitude_Altitude11, TheAltitude_Altitude10, TheAltitude_Altitude1)<=sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1))
TIME LIMIT: Killed by timeout after 3600 seconds
MemTotal: 16393916 kB
MemFree: 10752492 kB
After kill :
MemTotal: 16393916 kB
MemFree: 16179136 kB

BK_TIME_CONFINEMENT_REACHED

--------------------
content from stderr:

check for maximal unmarked siphon
ok
check for constant places
AltitudePossibleVal_Altitude1
AltitudePossibleVal_Altitude2
AltitudePossibleVal_Altitude3
AltitudePossibleVal_Altitude4
AltitudePossibleVal_Altitude5
AltitudePossibleVal_Altitude6
AltitudePossibleVal_Altitude7
AltitudePossibleVal_Altitude8
AltitudePossibleVal_Altitude9
AltitudePossibleVal_Altitude10
AltitudePossibleVal_Altitude11
AltitudePossibleVal_Altitude12
AltitudePossibleVal_Altitude13
AltitudePossibleVal_Altitude14
AltitudePossibleVal_Altitude15
AltitudePossibleVal_Altitude16
AltitudePossibleVal_Altitude17
AltitudePossibleVal_Altitude18
AltitudePossibleVal_Altitude19
AltitudePossibleVal_Altitude20
SpeedPossibleVal_Speed1
SpeedPossibleVal_Speed2
SpeedPossibleVal_Speed3
SpeedPossibleVal_Speed4
SpeedPossibleVal_Speed5
SpeedPossibleVal_Speed6
SpeedPossibleVal_Speed7
SpeedPossibleVal_Speed8
SpeedPossibleVal_Speed9
SpeedPossibleVal_Speed10
WeightPossibleVal_Weight0
WeightPossibleVal_Weight1
found 32 constant places
check if there are places and transitions
ok
check if there are transitions without pre-places
ok
check if at least one transition is enabled in m0
ok
check if there are transitions that can never fire
ok


initing FirstDep: 0m 0.001sec


iterations count:1219 (13), effective:54 (0)

initing FirstDep: 0m 0.000sec


iterations count:88 (1), effective:0 (0)

iterations count:88 (1), effective:0 (0)

iterations count:88 (1), effective:0 (0)

iterations count:88 (1), effective:0 (0)

iterations count:88 (1), effective:0 (0)

iterations count:38874 (441), effective:975 (11)

iterations count:88 (1), effective:0 (0)

iterations count:623 (7), effective:17 (0)

iterations count:88 (1), effective:0 (0)

iterations count:169 (1), effective:4 (0)

iterations count:88 (1), effective:0 (0)

iterations count:702 (7), effective:11 (0)

idd.h:1025: Timeout: after 598 sec


iterations count:89 (1), effective:1 (0)

iterations count:89 (1), effective:1 (0)

iterations count:89 (1), effective:1 (0)

iterations count:88 (1), effective:0 (0)

iterations count:88 (1), effective:0 (0)

iterations count:88 (1), effective:0 (0)

iterations count:88 (1), effective:0 (0)

iterations count:88 (1), effective:0 (0)

iterations count:88 (1), effective:0 (0)

iterations count:38874 (441), effective:975 (11)

iterations count:676 (7), effective:17 (0)

iterations count:88 (1), effective:0 (0)

iterations count:676 (7), effective:17 (0)

iterations count:88 (1), effective:0 (0)

iterations count:676 (7), effective:17 (0)

iterations count:88 (1), effective:0 (0)

iterations count:38846 (441), effective:971 (11)

idd.h:1025: Timeout: after 1486 sec

Sequence of Actions to be Executed by the VM

This is useful if one wants to reexecute the tool in the VM from the submitted image disk.

set -x
# this is for BenchKit: configuration of major elements for the test
export BK_INPUT="AirplaneLD-COL-0010"
export BK_EXAMINATION="CTLCardinality"
export BK_TOOL="marcie"
export BK_RESULT_DIR="/tmp/BK_RESULTS/OUTPUTS"
export BK_TIME_CONFINEMENT="3600"
export BK_MEMORY_CONFINEMENT="16384"
export BK_BIN_PATH="/home/mcc/BenchKit/bin/"

# this is specific to your benchmark or test

export BIN_DIR="$HOME/BenchKit/bin"

# remove the execution directoty if it exists (to avoid increse of .vmdk images)
if [ -d execution ] ; then
rm -rf execution
fi

# this is for BenchKit: explicit launching of the test
echo "====================================================================="
echo " Generated by BenchKit 2-5348"
echo " Executing tool marcie"
echo " Input is AirplaneLD-COL-0010, examination is CTLCardinality"
echo " Time confinement is $BK_TIME_CONFINEMENT seconds"
echo " Memory confinement is 16384 MBytes"
echo " Number of cores is 1"
echo " Run identifier is r001-oct2-167813588300169"
echo "====================================================================="
echo
echo "--------------------"
echo "preparation of the directory to be used:"

tar xzf /home/mcc/BenchKit/INPUTS/AirplaneLD-COL-0010.tgz
mv AirplaneLD-COL-0010 execution
cd execution
if [ "CTLCardinality" = "ReachabilityDeadlock" ] || [ "CTLCardinality" = "UpperBounds" ] || [ "CTLCardinality" = "QuasiLiveness" ] || [ "CTLCardinality" = "StableMarking" ] || [ "CTLCardinality" = "Liveness" ] || [ "CTLCardinality" = "OneSafe" ] || [ "CTLCardinality" = "StateSpace" ]; then
rm -f GenericPropertiesVerdict.xml
fi
pwd
ls -lh

echo
echo "--------------------"
echo "content from stdout:"
echo
echo "=== Data for post analysis generated by BenchKit (invocation template)"
echo
if [ "CTLCardinality" = "UpperBounds" ] ; then
echo "The expected result is a vector of positive values"
echo NUM_VECTOR
elif [ "CTLCardinality" != "StateSpace" ] ; then
echo "The expected result is a vector of booleans"
echo BOOL_VECTOR
else
echo "no data necessary for post analysis"
fi
echo
if [ -f "CTLCardinality.txt" ] ; then
echo "here is the order used to build the result vector(from text file)"
for x in $(grep Property CTLCardinality.txt | cut -d ' ' -f 2 | sort -u) ; do
echo "FORMULA_NAME $x"
done
elif [ -f "CTLCardinality.xml" ] ; then # for cunf (txt files deleted;-)
echo echo "here is the order used to build the result vector(from xml file)"
for x in $(grep '' CTLCardinality.xml | cut -d '>' -f 2 | cut -d '<' -f 1 | sort -u) ; do
echo "FORMULA_NAME $x"
done
elif [ "CTLCardinality" = "ReachabilityDeadlock" ] || [ "CTLCardinality" = "QuasiLiveness" ] || [ "CTLCardinality" = "StableMarking" ] || [ "CTLCardinality" = "Liveness" ] || [ "CTLCardinality" = "OneSafe" ] ; then
echo "FORMULA_NAME CTLCardinality"
fi
echo
echo "=== Now, execution of the tool begins"
echo
echo -n "BK_START "
date -u +%s%3N
echo
timeout -s 9 $BK_TIME_CONFINEMENT bash -c "/home/mcc/BenchKit/BenchKit_head.sh 2> STDERR ; echo ; echo -n \"BK_STOP \" ; date -u +%s%3N"
if [ $? -eq 137 ] ; then
echo
echo "BK_TIME_CONFINEMENT_REACHED"
fi
echo
echo "--------------------"
echo "content from stderr:"
echo
cat STDERR ;