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-oct2-167813588400241.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-PT-0010, examination is CTLCardinality
Time confinement is 3600 seconds
Memory confinement is 16384 MBytes
Number of cores is 1
Run identifier is r001-oct2-167813588400241
=====================================================================

--------------------
preparation of the directory to be used:
/home/mcc/execution
total 568K
-rw-r--r-- 1 mcc users 12K Feb 26 11:11 CTLCardinality.txt
-rw-r--r-- 1 mcc users 85K Feb 26 11:11 CTLCardinality.xml
-rw-r--r-- 1 mcc users 9.0K Feb 26 11:09 CTLFireability.txt
-rw-r--r-- 1 mcc users 68K Feb 26 11:09 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 6.2K Feb 25 15:30 LTLCardinality.txt
-rw-r--r-- 1 mcc users 31K Feb 25 15:30 LTLCardinality.xml
-rw-r--r-- 1 mcc users 4.3K Feb 25 15:30 LTLFireability.txt
-rw-r--r-- 1 mcc users 26K Feb 25 15:30 LTLFireability.xml
-rw-r--r-- 1 mcc users 17K Feb 26 11:14 ReachabilityCardinality.txt
-rw-r--r-- 1 mcc users 99K Feb 26 11:14 ReachabilityCardinality.xml
-rw-r--r-- 1 mcc users 13K Feb 26 11:13 ReachabilityFireability.txt
-rw-r--r-- 1 mcc users 89K Feb 26 11:13 ReachabilityFireability.xml
-rw-r--r-- 1 mcc users 1.8K Feb 25 15:30 UpperBounds.txt
-rw-r--r-- 1 mcc users 3.9K Feb 25 15:30 UpperBounds.xml
-rw-r--r-- 1 mcc users 5 Mar 5 18:22 equiv_col
-rw-r--r-- 1 mcc users 5 Mar 5 18:22 instance
-rw-r--r-- 1 mcc users 6 Mar 5 18:22 iscolored
-rw-r--r-- 1 mcc users 48K 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-PT-0010-CTLCardinality-00
FORMULA_NAME AirplaneLD-PT-0010-CTLCardinality-01
FORMULA_NAME AirplaneLD-PT-0010-CTLCardinality-02
FORMULA_NAME AirplaneLD-PT-0010-CTLCardinality-03
FORMULA_NAME AirplaneLD-PT-0010-CTLCardinality-04
FORMULA_NAME AirplaneLD-PT-0010-CTLCardinality-05
FORMULA_NAME AirplaneLD-PT-0010-CTLCardinality-06
FORMULA_NAME AirplaneLD-PT-0010-CTLCardinality-07
FORMULA_NAME AirplaneLD-PT-0010-CTLCardinality-08
FORMULA_NAME AirplaneLD-PT-0010-CTLCardinality-09
FORMULA_NAME AirplaneLD-PT-0010-CTLCardinality-10
FORMULA_NAME AirplaneLD-PT-0010-CTLCardinality-11
FORMULA_NAME AirplaneLD-PT-0010-CTLCardinality-12
FORMULA_NAME AirplaneLD-PT-0010-CTLCardinality-13
FORMULA_NAME AirplaneLD-PT-0010-CTLCardinality-14
FORMULA_NAME AirplaneLD-PT-0010-CTLCardinality-15

=== Now, execution of the tool begins

BK_START 1678387973392

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-PT-0010
Not applying reductions.
Model is PT
CTLCardinality PT
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

Net: AirplaneLD_PT_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 3.264sec


RS generation: 0m 0.022sec


-> reachability set: #nodes 1379 (1.4e+03) #states 43,463 (4)



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

checking: EF [~ [Speed_Left_Wheel_5<=1]]
normalized: E [true U ~ [Speed_Left_Wheel_5<=1]]

abstracting: (Speed_Left_Wheel_5<=1)
states: 43,463 (4)
-> the formula is FALSE

FORMULA AirplaneLD-PT-0010-CTLCardinality-09 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.001sec

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

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

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

MC time: 0m 0.027sec

checking: E [~ [1<=TheAltitude_6] U ~ [AX [~ [EG [EG [Speed_Left_Wheel_2<=1]]]]]]
normalized: E [~ [1<=TheAltitude_6] U EX [EG [EG [Speed_Left_Wheel_2<=1]]]]

abstracting: (Speed_Left_Wheel_2<=1)
states: 43,463 (4)

EG iterations: 0

EG iterations: 0
.abstracting: (1<=TheAltitude_6)
states: 2,057 (3)
-> the formula is TRUE

FORMULA AirplaneLD-PT-0010-CTLCardinality-11 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.024sec

checking: [AF [56<=stp1] & AF [~ [[63<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on) & AF [~ [AF [sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)<=71]]]]]]]
normalized: [~ [EG [[63<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on) & ~ [EG [~ [EG [~ [sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)<=71]]]]]]]] & ~ [EG [~ [56<=stp1]]]]

abstracting: (56<=stp1)
states: 0

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

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

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

MC time: 0m 0.051sec

checking: EG [EF [AF [E [[P2<=Speed_Left_Wheel_1 | SpeedPossibleVal_7<=0] U ~ [Plane_On_Ground_Signal_no_F<=AltitudePossibleVal_11]]]]]
normalized: EG [E [true U ~ [EG [~ [E [[P2<=Speed_Left_Wheel_1 | SpeedPossibleVal_7<=0] U ~ [Plane_On_Ground_Signal_no_F<=AltitudePossibleVal_11]]]]]]]

abstracting: (Plane_On_Ground_Signal_no_F<=AltitudePossibleVal_11)
states: 43,463 (4)
abstracting: (SpeedPossibleVal_7<=0)
states: 0
abstracting: (P2<=Speed_Left_Wheel_1)
states: 36,533 (4)

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

FORMULA AirplaneLD-PT-0010-CTLCardinality-14 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.002sec

checking: A [P2<=stp3 U [EG [[EG [AF [stp5<=2]] & stp2<=92]] | AF [AG [[33<=P3 & AF [P3<=17]]]]]]
normalized: [~ [EG [~ [[~ [EG [E [true U ~ [[~ [EG [~ [P3<=17]]] & 33<=P3]]]]] | EG [[EG [~ [EG [~ [stp5<=2]]]] & stp2<=92]]]]]] & ~ [E [~ [[~ [EG [E [true U ~ [[~ [EG [~ [P3<=17]]] & 33<=P3]]]]] | EG [[EG [~ [EG [~ [stp5<=2]]]] & stp2<=92]]]] U [~ [P2<=stp3] & ~ [[~ [EG [E [true U ~ [[~ [EG [~ [P3<=17]]] & 33<=P3]]]]] | EG [[EG [~ [EG [~ [stp5<=2]]]] & stp2<=92]]]]]]]]

abstracting: (stp2<=92)
states: 43,463 (4)
abstracting: (stp5<=2)
states: 43,463 (4)
.
EG iterations: 1

EG iterations: 0

EG iterations: 0
abstracting: (33<=P3)
states: 0
abstracting: (P3<=17)
states: 43,463 (4)
.
EG iterations: 1

EG iterations: 0
abstracting: (P2<=stp3)
states: 36,203 (4)
abstracting: (stp2<=92)
states: 43,463 (4)
abstracting: (stp5<=2)
states: 43,463 (4)
.
EG iterations: 1

EG iterations: 0

EG iterations: 0
abstracting: (33<=P3)
states: 0
abstracting: (P3<=17)
states: 43,463 (4)
.
EG iterations: 1

EG iterations: 0
abstracting: (stp2<=92)
states: 43,463 (4)
abstracting: (stp5<=2)
states: 43,463 (4)
.
EG iterations: 1

EG iterations: 0

EG iterations: 0
abstracting: (33<=P3)
states: 0
abstracting: (P3<=17)
states: 43,463 (4)
.
EG iterations: 1

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

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

MC time: 0m 0.006sec

checking: E [AF [[EX [A [P3<=19 U P2<=P2]] | AX [76<=stp1]]] U AG [AX [EG [sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)<=P1]]]]
normalized: E [~ [EG [~ [[~ [EX [~ [76<=stp1]]] | EX [[~ [EG [~ [P2<=P2]]] & ~ [E [~ [P2<=P2] U [~ [P3<=19] & ~ [P2<=P2]]]]]]]]]] U ~ [E [true U EX [~ [EG [sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)<=P1]]]]]]

abstracting: (sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)<=P1)
states: 33,165 (4)
...........
EG iterations: 11
.abstracting: (P2<=P2)
states: 43,463 (4)
abstracting: (P3<=19)
states: 43,463 (4)
abstracting: (P2<=P2)
states: 43,463 (4)
abstracting: (P2<=P2)
states: 43,463 (4)
.
EG iterations: 1
.abstracting: (76<=stp1)
states: 0
..
EG iterations: 1
-> the formula is TRUE

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

MC time: 0m 0.371sec

checking: ~ [EF [EX [[[[TheAltitude_20<=AltitudePossibleVal_4 | AltitudePossibleVal_2<=1] | A [TheAltitude_12<=TheAltitude_3 U Speed_Right_Wheel_5<=0]] & ~ [AF [TheAltitude_17<=1]]]]]]
normalized: ~ [E [true U EX [[[[~ [E [~ [Speed_Right_Wheel_5<=0] U [~ [TheAltitude_12<=TheAltitude_3] & ~ [Speed_Right_Wheel_5<=0]]]] & ~ [EG [~ [Speed_Right_Wheel_5<=0]]]] | [TheAltitude_20<=AltitudePossibleVal_4 | AltitudePossibleVal_2<=1]] & EG [~ [TheAltitude_17<=1]]]]]]

abstracting: (TheAltitude_17<=1)
states: 43,463 (4)
.
EG iterations: 1
abstracting: (AltitudePossibleVal_2<=1)
states: 43,463 (4)
abstracting: (TheAltitude_20<=AltitudePossibleVal_4)
states: 43,463 (4)
abstracting: (Speed_Right_Wheel_5<=0)
states: 39,512 (4)
......
EG iterations: 6
abstracting: (Speed_Right_Wheel_5<=0)
states: 39,512 (4)
abstracting: (TheAltitude_12<=TheAltitude_3)
states: 41,406 (4)
abstracting: (Speed_Right_Wheel_5<=0)
states: 39,512 (4)
.-> the formula is TRUE

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

MC time: 0m 0.013sec

checking: A [[EF [[[AG [WeightPossibleVal_on<=1] & ~ [[AltitudePossibleVal_11<=1 | TheAltitude_11<=1]]] & [EX [1<=TheAltitude_10] | AltitudePossibleVal_6<=AltitudePossibleVal_18]]] & ~ [EF [~ [[1<=Speed_Left_Wheel_4 | WeightPossibleVal_on<=AltitudePossibleVal_3]]]]] U EX [AF [EF [AG [SpeedPossibleVal_6<=0]]]]]
normalized: [~ [E [~ [EX [~ [EG [~ [E [true U ~ [E [true U ~ [SpeedPossibleVal_6<=0]]]]]]]]] U [~ [[~ [E [true U ~ [[1<=Speed_Left_Wheel_4 | WeightPossibleVal_on<=AltitudePossibleVal_3]]]] & E [true U [[EX [1<=TheAltitude_10] | AltitudePossibleVal_6<=AltitudePossibleVal_18] & [~ [[AltitudePossibleVal_11<=1 | TheAltitude_11<=1]] & ~ [E [true U ~ [WeightPossibleVal_on<=1]]]]]]]] & ~ [EX [~ [EG [~ [E [true U ~ [E [true U ~ [SpeedPossibleVal_6<=0]]]]]]]]]]]] & ~ [EG [~ [EX [~ [EG [~ [E [true U ~ [E [true U ~ [SpeedPossibleVal_6<=0]]]]]]]]]]]]

abstracting: (SpeedPossibleVal_6<=0)
states: 0

EG iterations: 0
.
EG iterations: 0
abstracting: (SpeedPossibleVal_6<=0)
states: 0

EG iterations: 0
.abstracting: (WeightPossibleVal_on<=1)
states: 43,463 (4)
abstracting: (TheAltitude_11<=1)
states: 43,463 (4)
abstracting: (AltitudePossibleVal_11<=1)
states: 43,463 (4)
abstracting: (AltitudePossibleVal_6<=AltitudePossibleVal_18)
states: 43,463 (4)
abstracting: (1<=TheAltitude_10)
states: 2,057 (3)
.abstracting: (WeightPossibleVal_on<=AltitudePossibleVal_3)
states: 43,463 (4)
abstracting: (1<=Speed_Left_Wheel_4)
states: 3,949 (3)
abstracting: (SpeedPossibleVal_6<=0)
states: 0

EG iterations: 0
.-> the formula is FALSE

FORMULA AirplaneLD-PT-0010-CTLCardinality-15 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.012sec

checking: [~ [E [E [AltitudePossibleVal_6<=AltitudePossibleVal_2 U E [E [Weight_Right_Wheel_on<=0 U AltitudePossibleVal_13<=0] U ~ [TheAltitude_15<=P4]]] U ~ [EF [~ [[stp5<=1 & 1<=P3]]]]]] & EG [[P5<=1 | [1<=P5 | EG [[Weight_Left_Wheel_off<=AltitudePossibleVal_15 & [1<=AltitudePossibleVal_11 | P4<=1]]]]]]]
normalized: [EG [[P5<=1 | [1<=P5 | EG [[Weight_Left_Wheel_off<=AltitudePossibleVal_15 & [1<=AltitudePossibleVal_11 | P4<=1]]]]]] & ~ [E [E [AltitudePossibleVal_6<=AltitudePossibleVal_2 U E [E [Weight_Right_Wheel_on<=0 U AltitudePossibleVal_13<=0] U ~ [TheAltitude_15<=P4]]] U ~ [E [true U ~ [[stp5<=1 & 1<=P3]]]]]]]

abstracting: (1<=P3)
states: 2,541 (3)
abstracting: (stp5<=1)
states: 43,463 (4)
abstracting: (TheAltitude_15<=P4)
states: 41,406 (4)
abstracting: (AltitudePossibleVal_13<=0)
states: 0
abstracting: (Weight_Right_Wheel_on<=0)
states: 30,758 (4)
abstracting: (AltitudePossibleVal_6<=AltitudePossibleVal_2)
states: 43,463 (4)
abstracting: (P4<=1)
states: 43,463 (4)
abstracting: (1<=AltitudePossibleVal_11)
states: 43,463 (4)
abstracting: (Weight_Left_Wheel_off<=AltitudePossibleVal_15)
states: 43,463 (4)

EG iterations: 0
abstracting: (1<=P5)
states: 11
abstracting: (P5<=1)
states: 43,463 (4)

EG iterations: 0
-> the formula is TRUE

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

MC time: 0m 0.020sec

checking: A [A [AG [~ [AltitudePossibleVal_15<=0]] U P5<=0] U ~ [[SpeedPossibleVal_10<=SpeedPossibleVal_10 | A [[E [P6<=AltitudePossibleVal_15 U TheAltitude_2<=0] & P4<=P1] U ~ [[A [Speed_Right_Wheel_1<=AltitudePossibleVal_20 U P3<=0] & [SpeedPossibleVal_5<=TheAltitude_11 | AltitudePossibleVal_12<=0]]]]]]]
normalized: [~ [EG [[SpeedPossibleVal_10<=SpeedPossibleVal_10 | [~ [EG [[[SpeedPossibleVal_5<=TheAltitude_11 | AltitudePossibleVal_12<=0] & [~ [EG [~ [P3<=0]]] & ~ [E [~ [P3<=0] U [~ [Speed_Right_Wheel_1<=AltitudePossibleVal_20] & ~ [P3<=0]]]]]]]] & ~ [E [[[SpeedPossibleVal_5<=TheAltitude_11 | AltitudePossibleVal_12<=0] & [~ [EG [~ [P3<=0]]] & ~ [E [~ [P3<=0] U [~ [Speed_Right_Wheel_1<=AltitudePossibleVal_20] & ~ [P3<=0]]]]]] U [~ [[P4<=P1 & E [P6<=AltitudePossibleVal_15 U TheAltitude_2<=0]]] & [[SpeedPossibleVal_5<=TheAltitude_11 | AltitudePossibleVal_12<=0] & [~ [EG [~ [P3<=0]]] & ~ [E [~ [P3<=0] U [~ [Speed_Right_Wheel_1<=AltitudePossibleVal_20] & ~ [P3<=0]]]]]]]]]]]]] & ~ [E [[SpeedPossibleVal_10<=SpeedPossibleVal_10 | [~ [EG [[[SpeedPossibleVal_5<=TheAltitude_11 | AltitudePossibleVal_12<=0] & [~ [EG [~ [P3<=0]]] & ~ [E [~ [P3<=0] U [~ [Speed_Right_Wheel_1<=AltitudePossibleVal_20] & ~ [P3<=0]]]]]]]] & ~ [E [[[SpeedPossibleVal_5<=TheAltitude_11 | AltitudePossibleVal_12<=0] & [~ [EG [~ [P3<=0]]] & ~ [E [~ [P3<=0] U [~ [Speed_Right_Wheel_1<=AltitudePossibleVal_20] & ~ [P3<=0]]]]]] U [~ [[P4<=P1 & E [P6<=AltitudePossibleVal_15 U TheAltitude_2<=0]]] & [[SpeedPossibleVal_5<=TheAltitude_11 | AltitudePossibleVal_12<=0] & [~ [EG [~ [P3<=0]]] & ~ [E [~ [P3<=0] U [~ [Speed_Right_Wheel_1<=AltitudePossibleVal_20] & ~ [P3<=0]]]]]]]]]]] U [~ [[~ [EG [~ [P5<=0]]] & ~ [E [~ [P5<=0] U [E [true U AltitudePossibleVal_15<=0] & ~ [P5<=0]]]]]] & [SpeedPossibleVal_10<=SpeedPossibleVal_10 | [~ [EG [[[SpeedPossibleVal_5<=TheAltitude_11 | AltitudePossibleVal_12<=0] & [~ [EG [~ [P3<=0]]] & ~ [E [~ [P3<=0] U [~ [Speed_Right_Wheel_1<=AltitudePossibleVal_20] & ~ [P3<=0]]]]]]]] & ~ [E [[[SpeedPossibleVal_5<=TheAltitude_11 | AltitudePossibleVal_12<=0] & [~ [EG [~ [P3<=0]]] & ~ [E [~ [P3<=0] U [~ [Speed_Right_Wheel_1<=AltitudePossibleVal_20] & ~ [P3<=0]]]]]] U [~ [[P4<=P1 & E [P6<=AltitudePossibleVal_15 U TheAltitude_2<=0]]] & [[SpeedPossibleVal_5<=TheAltitude_11 | AltitudePossibleVal_12<=0] & [~ [EG [~ [P3<=0]]] & ~ [E [~ [P3<=0] U [~ [Speed_Right_Wheel_1<=AltitudePossibleVal_20] & ~ [P3<=0]]]]]]]]]]]]]]]

abstracting: (P3<=0)
states: 40,922 (4)
abstracting: (Speed_Right_Wheel_1<=AltitudePossibleVal_20)
states: 43,463 (4)
abstracting: (P3<=0)
states: 40,922 (4)
abstracting: (P3<=0)
states: 40,922 (4)
.....
EG iterations: 5
abstracting: (AltitudePossibleVal_12<=0)
states: 0
abstracting: (SpeedPossibleVal_5<=TheAltitude_11)
states: 2,057 (3)
abstracting: (TheAltitude_2<=0)
states: 41,406 (4)
abstracting: (P6<=AltitudePossibleVal_15)
states: 43,463 (4)
abstracting: (P4<=P1)
states: 43,342 (4)
abstracting: (P3<=0)
states: 40,922 (4)
abstracting: (Speed_Right_Wheel_1<=AltitudePossibleVal_20)
states: 43,463 (4)
abstracting: (P3<=0)
states: 40,922 (4)
abstracting: (P3<=0)
states: 40,922 (4)
.....
EG iterations: 5
abstracting: (AltitudePossibleVal_12<=0)
states: 0
abstracting: (SpeedPossibleVal_5<=TheAltitude_11)
states: 2,057 (3)
abstracting: (P3<=0)
states: 40,922 (4)
abstracting: (Speed_Right_Wheel_1<=AltitudePossibleVal_20)
states: 43,463 (4)
abstracting: (P3<=0)
states: 40,922 (4)
abstracting: (P3<=0)
states: 40,922 (4)
.....
EG iterations: 5
abstracting: (AltitudePossibleVal_12<=0)
states: 0
abstracting: (SpeedPossibleVal_5<=TheAltitude_11)
states: 2,057 (3)
......
EG iterations: 6
abstracting: (SpeedPossibleVal_10<=SpeedPossibleVal_10)
states: 43,463 (4)
abstracting: (P5<=0)
states: 43,452 (4)
abstracting: (AltitudePossibleVal_15<=0)
states: 0
abstracting: (P5<=0)
states: 43,452 (4)
abstracting: (P5<=0)
states: 43,452 (4)
...
EG iterations: 3
abstracting: (P3<=0)
states: 40,922 (4)
abstracting: (Speed_Right_Wheel_1<=AltitudePossibleVal_20)
states: 43,463 (4)
abstracting: (P3<=0)
states: 40,922 (4)
abstracting: (P3<=0)
states: 40,922 (4)
.....
EG iterations: 5
abstracting: (AltitudePossibleVal_12<=0)
states: 0
abstracting: (SpeedPossibleVal_5<=TheAltitude_11)
states: 2,057 (3)
abstracting: (TheAltitude_2<=0)
states: 41,406 (4)
abstracting: (P6<=AltitudePossibleVal_15)
states: 43,463 (4)
abstracting: (P4<=P1)
states: 43,342 (4)
abstracting: (P3<=0)
states: 40,922 (4)
abstracting: (Speed_Right_Wheel_1<=AltitudePossibleVal_20)
states: 43,463 (4)
abstracting: (P3<=0)
states: 40,922 (4)
abstracting: (P3<=0)
states: 40,922 (4)
.....
EG iterations: 5
abstracting: (AltitudePossibleVal_12<=0)
states: 0
abstracting: (SpeedPossibleVal_5<=TheAltitude_11)
states: 2,057 (3)
abstracting: (P3<=0)
states: 40,922 (4)
abstracting: (Speed_Right_Wheel_1<=AltitudePossibleVal_20)
states: 43,463 (4)
abstracting: (P3<=0)
states: 40,922 (4)
abstracting: (P3<=0)
states: 40,922 (4)
.....
EG iterations: 5
abstracting: (AltitudePossibleVal_12<=0)
states: 0
abstracting: (SpeedPossibleVal_5<=TheAltitude_11)
states: 2,057 (3)
......
EG iterations: 6
abstracting: (SpeedPossibleVal_10<=SpeedPossibleVal_10)
states: 43,463 (4)
abstracting: (P3<=0)
states: 40,922 (4)
abstracting: (Speed_Right_Wheel_1<=AltitudePossibleVal_20)
states: 43,463 (4)
abstracting: (P3<=0)
states: 40,922 (4)
abstracting: (P3<=0)
states: 40,922 (4)
.....
EG iterations: 5
abstracting: (AltitudePossibleVal_12<=0)
states: 0
abstracting: (SpeedPossibleVal_5<=TheAltitude_11)
states: 2,057 (3)
abstracting: (TheAltitude_2<=0)
states: 41,406 (4)
abstracting: (P6<=AltitudePossibleVal_15)
states: 43,463 (4)
abstracting: (P4<=P1)
states: 43,342 (4)
abstracting: (P3<=0)
states: 40,922 (4)
abstracting: (Speed_Right_Wheel_1<=AltitudePossibleVal_20)
states: 43,463 (4)
abstracting: (P3<=0)
states: 40,922 (4)
abstracting: (P3<=0)
states: 40,922 (4)
.....
EG iterations: 5
abstracting: (AltitudePossibleVal_12<=0)
states: 0
abstracting: (SpeedPossibleVal_5<=TheAltitude_11)
states: 2,057 (3)
abstracting: (P3<=0)
states: 40,922 (4)
abstracting: (Speed_Right_Wheel_1<=AltitudePossibleVal_20)
states: 43,463 (4)
abstracting: (P3<=0)
states: 40,922 (4)
abstracting: (P3<=0)
states: 40,922 (4)
.....
EG iterations: 5
abstracting: (AltitudePossibleVal_12<=0)
states: 0
abstracting: (SpeedPossibleVal_5<=TheAltitude_11)
states: 2,057 (3)
......
EG iterations: 6
abstracting: (SpeedPossibleVal_10<=SpeedPossibleVal_10)
states: 43,463 (4)

EG iterations: 0
-> the formula is FALSE

FORMULA AirplaneLD-PT-0010-CTLCardinality-13 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.024sec

checking: [E [[EG [SpeedPossibleVal_4<=TheAltitude_7] & E [EF [TheAltitude_4<=AltitudePossibleVal_2] U ~ [[1<=WeightPossibleVal_off | [TheAltitude_15<=SpeedPossibleVal_3 & Speed_Left_Wheel_1<=0]]]]] U AF [EF [~ [[stp4<=Weight_Left_Wheel_off & SpeedPossibleVal_10<=Speed_Left_Wheel_1]]]]] & EX [A [AG [~ [A [Speed_Left_Wheel_5<=1 U Speed_Left_Wheel_3<=AltitudePossibleVal_16]]] U A [[AF [1<=P1] | [TheAltitude_14<=Speed_Right_Wheel_4 | TheAltitude_18<=Speed_Right_Wheel_6]] U EG [AltitudePossibleVal_3<=0]]]]]
normalized: [E [[E [E [true U TheAltitude_4<=AltitudePossibleVal_2] U ~ [[[TheAltitude_15<=SpeedPossibleVal_3 & Speed_Left_Wheel_1<=0] | 1<=WeightPossibleVal_off]]] & EG [SpeedPossibleVal_4<=TheAltitude_7]] U ~ [EG [~ [E [true U ~ [[stp4<=Weight_Left_Wheel_off & SpeedPossibleVal_10<=Speed_Left_Wheel_1]]]]]]] & EX [[~ [EG [~ [[~ [EG [~ [EG [AltitudePossibleVal_3<=0]]]] & ~ [E [~ [EG [AltitudePossibleVal_3<=0]] U [~ [EG [AltitudePossibleVal_3<=0]] & ~ [[[TheAltitude_14<=Speed_Right_Wheel_4 | TheAltitude_18<=Speed_Right_Wheel_6] | ~ [EG [~ [1<=P1]]]]]]]]]]]] & ~ [E [~ [[~ [EG [~ [EG [AltitudePossibleVal_3<=0]]]] & ~ [E [~ [EG [AltitudePossibleVal_3<=0]] U [~ [EG [AltitudePossibleVal_3<=0]] & ~ [[[TheAltitude_14<=Speed_Right_Wheel_4 | TheAltitude_18<=Speed_Right_Wheel_6] | ~ [EG [~ [1<=P1]]]]]]]]]] U [~ [[~ [EG [~ [EG [AltitudePossibleVal_3<=0]]]] & ~ [E [~ [EG [AltitudePossibleVal_3<=0]] U [~ [EG [AltitudePossibleVal_3<=0]] & ~ [[[TheAltitude_14<=Speed_Right_Wheel_4 | TheAltitude_18<=Speed_Right_Wheel_6] | ~ [EG [~ [1<=P1]]]]]]]]]] & E [true U [~ [EG [~ [Speed_Left_Wheel_3<=AltitudePossibleVal_16]]] & ~ [E [~ [Speed_Left_Wheel_3<=AltitudePossibleVal_16] U [~ [Speed_Left_Wheel_5<=1] & ~ [Speed_Left_Wheel_3<=AltitudePossibleVal_16]]]]]]]]]]]]

abstracting: (Speed_Left_Wheel_3<=AltitudePossibleVal_16)
states: 43,463 (4)
abstracting: (Speed_Left_Wheel_5<=1)
states: 43,463 (4)
abstracting: (Speed_Left_Wheel_3<=AltitudePossibleVal_16)
states: 43,463 (4)
abstracting: (Speed_Left_Wheel_3<=AltitudePossibleVal_16)
states: 43,463 (4)
.
EG iterations: 1
abstracting: (1<=P1)
states: 22,869 (4)
.
EG iterations: 1
abstracting: (TheAltitude_18<=Speed_Right_Wheel_6)
states: 41,593 (4)
abstracting: (TheAltitude_14<=Speed_Right_Wheel_4)
states: 41,593 (4)
abstracting: (AltitudePossibleVal_3<=0)
states: 0
.
EG iterations: 1
abstracting: (AltitudePossibleVal_3<=0)
states: 0
.
EG iterations: 1
abstracting: (AltitudePossibleVal_3<=0)
states: 0
.
EG iterations: 1

EG iterations: 0
abstracting: (1<=P1)
states: 22,869 (4)
.
EG iterations: 1
abstracting: (TheAltitude_18<=Speed_Right_Wheel_6)
states: 41,593 (4)
abstracting: (TheAltitude_14<=Speed_Right_Wheel_4)
states: 41,593 (4)
abstracting: (AltitudePossibleVal_3<=0)
states: 0
.
EG iterations: 1
abstracting: (AltitudePossibleVal_3<=0)
states: 0
.
EG iterations: 1
abstracting: (AltitudePossibleVal_3<=0)
states: 0
.
EG iterations: 1

EG iterations: 0
abstracting: (1<=P1)
states: 22,869 (4)
.
EG iterations: 1
abstracting: (TheAltitude_18<=Speed_Right_Wheel_6)
states: 41,593 (4)
abstracting: (TheAltitude_14<=Speed_Right_Wheel_4)
states: 41,593 (4)
abstracting: (AltitudePossibleVal_3<=0)
states: 0
.
EG iterations: 1
abstracting: (AltitudePossibleVal_3<=0)
states: 0
.
EG iterations: 1
abstracting: (AltitudePossibleVal_3<=0)
states: 0
.
EG iterations: 1

EG iterations: 0

EG iterations: 0
.abstracting: (SpeedPossibleVal_10<=Speed_Left_Wheel_1)
states: 3,949 (3)
abstracting: (stp4<=Weight_Left_Wheel_off)
states: 40,207 (4)
.
EG iterations: 1
abstracting: (SpeedPossibleVal_4<=TheAltitude_7)
states: 2,057 (3)
......
EG iterations: 6
abstracting: (1<=WeightPossibleVal_off)
states: 43,463 (4)
abstracting: (Speed_Left_Wheel_1<=0)
states: 39,514 (4)
abstracting: (TheAltitude_15<=SpeedPossibleVal_3)
states: 43,463 (4)
abstracting: (TheAltitude_4<=AltitudePossibleVal_2)
states: 43,463 (4)
-> the formula is FALSE

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

MC time: 0m 0.044sec

checking: EX [AG [[~ [EG [[sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=35 | sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=59]]] | A [P3<=P6 U 53<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1)]]]]
normalized: EX [~ [E [true U ~ [[[~ [EG [~ [53<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1)]]] & ~ [E [~ [53<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1)] U [~ [53<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1)] & ~ [P3<=P6]]]]] | ~ [EG [[sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=35 | sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=59]]]]]]]]

abstracting: (sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=59)
states: 43,463 (4)
abstracting: (sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=35)
states: 43,463 (4)

EG iterations: 0
abstracting: (P3<=P6)
states: 40,922 (4)
abstracting: (53<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1))
states: 0
abstracting: (53<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1))
states: 0
abstracting: (53<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1))
states: 0

EG iterations: 0
.-> the formula is FALSE

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

MC time: 0m 2.389sec

checking: ~ [[EF [[[[P4<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T) & P4<=stp2] & ~ [E [stp1<=71 U 42<=stp3]]] & sum(WeightPossibleVal_off, WeightPossibleVal_on)<=3]] | [EG [EG [EG [26<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)]]] & EF [E [EX [sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)<=sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)] U [AX [P5<=19] & 53<=sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)]]]]]]
normalized: ~ [[E [true U [sum(WeightPossibleVal_off, WeightPossibleVal_on)<=3 & [~ [E [stp1<=71 U 42<=stp3]] & [P4<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T) & P4<=stp2]]]] | [EG [EG [EG [26<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)]]] & E [true U E [EX [sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)<=sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)] U [53<=sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1) & ~ [EX [~ [P5<=19]]]]]]]]]

abstracting: (P5<=19)
states: 43,463 (4)
.abstracting: (53<=sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1))
states: 0
abstracting: (sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)<=sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on))
states: 38,381 (4)
.abstracting: (26<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on))
states: 0
.
EG iterations: 1
.
EG iterations: 1
.
EG iterations: 1
abstracting: (P4<=stp2)
states: 43,342 (4)
abstracting: (P4<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T))
states: 43,342 (4)
abstracting: (42<=stp3)
states: 0
abstracting: (stp1<=71)
states: 43,463 (4)
abstracting: (sum(WeightPossibleVal_off, WeightPossibleVal_on)<=3)
states: 43,463 (4)
-> the formula is FALSE

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

MC time: 0m 2.366sec

checking: E [[AG [[EF [[52<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T) | sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)<=P1]] & E [[79<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T) | stp5<=P6] U stp3<=92]]] | ~ [[~ [EG [P3<=stp5]] & [~ [P5<=51] & ~ [[sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=58 & sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)<=94]]]]]] U A [~ [P5<=41] U [[AG [[stp1<=14 | sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)<=54]] & [sum(WeightPossibleVal_off, WeightPossibleVal_on)<=19 & [stp2<=sum(WeightPossibleVal_off, WeightPossibleVal_on) | ~ [stp4<=P3]]]] & AX [[14<=P4 & [sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T) & 39<=stp1]]]]]]
normalized: E [[~ [E [true U ~ [[E [true U [52<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T) | sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)<=P1]] & E [[79<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T) | stp5<=P6] U stp3<=92]]]]] | ~ [[[~ [[sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=58 & sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)<=94]] & ~ [P5<=51]] & ~ [EG [P3<=stp5]]]]] U [~ [E [~ [[[[sum(WeightPossibleVal_off, WeightPossibleVal_on)<=19 & [stp2<=sum(WeightPossibleVal_off, WeightPossibleVal_on) | ~ [stp4<=P3]]] & ~ [E [true U ~ [[stp1<=14 | sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)<=54]]]]] & ~ [EX [~ [[14<=P4 & [sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T) & 39<=stp1]]]]]]] U [P5<=41 & ~ [[[[sum(WeightPossibleVal_off, WeightPossibleVal_on)<=19 & [stp2<=sum(WeightPossibleVal_off, WeightPossibleVal_on) | ~ [stp4<=P3]]] & ~ [E [true U ~ [[stp1<=14 | sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)<=54]]]]] & ~ [EX [~ [[14<=P4 & [sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T) & 39<=stp1]]]]]]]]]] & ~ [EG [~ [[[[sum(WeightPossibleVal_off, WeightPossibleVal_on)<=19 & [stp2<=sum(WeightPossibleVal_off, WeightPossibleVal_on) | ~ [stp4<=P3]]] & ~ [E [true U ~ [[stp1<=14 | sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)<=54]]]]] & ~ [EX [~ [[14<=P4 & [sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T) & 39<=stp1]]]]]]]]]]]

abstracting: (39<=stp1)
states: 0
abstracting: (sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T))
states: 0
abstracting: (14<=P4)
states: 0
.abstracting: (sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)<=54)
states: 43,463 (4)
abstracting: (stp1<=14)
states: 43,463 (4)
abstracting: (stp4<=P3)
states: 39,745 (4)
abstracting: (stp2<=sum(WeightPossibleVal_off, WeightPossibleVal_on))
states: 43,463 (4)
abstracting: (sum(WeightPossibleVal_off, WeightPossibleVal_on)<=19)
states: 43,463 (4)
...........
EG iterations: 11
abstracting: (39<=stp1)
states: 0
abstracting: (sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T))
states: 0
abstracting: (14<=P4)
states: 0
.abstracting: (sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)<=54)
states: 43,463 (4)
abstracting: (stp1<=14)
states: 43,463 (4)
abstracting: (stp4<=P3)
states: 39,745 (4)
abstracting: (stp2<=sum(WeightPossibleVal_off, WeightPossibleVal_on))
states: 43,463 (4)
abstracting: (sum(WeightPossibleVal_off, WeightPossibleVal_on)<=19)
states: 43,463 (4)
abstracting: (P5<=41)
states: 43,463 (4)
abstracting: (39<=stp1)
states: 0
abstracting: (sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T))
states: 0
abstracting: (14<=P4)
states: 0
.abstracting: (sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)<=54)
states: 43,463 (4)
abstracting: (stp1<=14)
states: 43,463 (4)
abstracting: (stp4<=P3)
states: 39,745 (4)
abstracting: (stp2<=sum(WeightPossibleVal_off, WeightPossibleVal_on))
states: 43,463 (4)
abstracting: (sum(WeightPossibleVal_off, WeightPossibleVal_on)<=19)
states: 43,463 (4)
abstracting: (P3<=stp5)
states: 41,153 (4)
.....
EG iterations: 5
abstracting: (P5<=51)
states: 43,463 (4)
abstracting: (sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)<=94)
states: 43,463 (4)
abstracting: (sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=58)
states: 43,463 (4)
abstracting: (stp3<=92)
states: 43,463 (4)
abstracting: (stp5<=P6)
states: 40,448 (4)
abstracting: (79<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T))
states: 0
abstracting: (sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)<=P1)
states: 0
abstracting: (52<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T))
states: 0
-> the formula is TRUE

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

MC time: 0m 9.358sec

checking: A [E [~ [76<=stp5] U ~ [[AF [[sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=89 | stp3<=sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)]] | [[A [42<=stp1 U 81<=P4] & ~ [27<=stp4]] | [EX [P3<=55] & [stp1<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T) | sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)<=13]]]]]] U EG [[[stp2<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1) & ~ [[~ [sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=25] | ~ [sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1)<=62]]]] & EF [EX [sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)]]]]]
normalized: [~ [EG [~ [EG [[[stp2<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1) & ~ [[~ [sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=25] | ~ [sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1)<=62]]]] & E [true U EX [sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)]]]]]]] & ~ [E [~ [EG [[[stp2<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1) & ~ [[~ [sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=25] | ~ [sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1)<=62]]]] & E [true U EX [sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)]]]]] U [~ [EG [[[stp2<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1) & ~ [[~ [sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=25] | ~ [sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1)<=62]]]] & E [true U EX [sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)]]]]] & ~ [E [~ [76<=stp5] U ~ [[[[[stp1<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T) | sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)<=13] & EX [P3<=55]] | [~ [27<=stp4] & [~ [EG [~ [81<=P4]]] & ~ [E [~ [81<=P4] U [~ [42<=stp1] & ~ [81<=P4]]]]]]] | ~ [EG [~ [[sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=89 | stp3<=sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)]]]]]]]]]]]]

abstracting: (stp3<=sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1))
states: 43,463 (4)
abstracting: (sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=89)
states: 43,463 (4)
.
EG iterations: 1
abstracting: (81<=P4)
states: 0
abstracting: (42<=stp1)
states: 0
abstracting: (81<=P4)
states: 0
abstracting: (81<=P4)
states: 0

EG iterations: 0
abstracting: (27<=stp4)
states: 0
abstracting: (P3<=55)
states: 43,463 (4)
.abstracting: (sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)<=13)
states: 43,463 (4)
abstracting: (stp1<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T))
states: 35,840 (4)
abstracting: (76<=stp5)
states: 0
abstracting: (sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T))
states: 13,323 (4)
.abstracting: (sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1)<=62)
states: 43,463 (4)
abstracting: (sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=25)
states: 43,463 (4)
abstracting: (stp2<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1))
states: 42,308 (4)
..........
EG iterations: 10
abstracting: (sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T))
states: 13,323 (4)
.abstracting: (sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1)<=62)
states: 43,463 (4)
abstracting: (sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=25)
states: 43,463 (4)
abstracting: (stp2<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1))
states: 42,308 (4)
..........
EG iterations: 10
abstracting: (sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T))
states: 13,323 (4)
.abstracting: (sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1)<=62)
states: 43,463 (4)
abstracting: (sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=25)
states: 43,463 (4)
abstracting: (stp2<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1))
states: 42,308 (4)
..........
EG iterations: 10

EG iterations: 0
-> the formula is FALSE

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

MC time: 0m 1.137sec

totally nodes used: 112048 (1.1e+05)
number of garbage collections: 0
fire ops cache: hits/miss/sum: 950239 1717626 2667865
used/not used/entry size/cache size: 1738551 65370313 16 1024MB
basic ops cache: hits/miss/sum: 155681 186276 341957
used/not used/entry size/cache size: 286133 16491083 12 192MB
unary ops cache: hits/miss/sum: 0 0 0
used/not used/entry size/cache size: 0 16777216 8 128MB
abstract ops cache: hits/miss/sum: 0 8398927 8398927
used/not used/entry size/cache size: 1 16777215 12 192MB
state nr cache: hits/miss/sum: 4678 9161 13839
used/not used/entry size/cache size: 9159 8379449 32 256MB
max state cache: hits/miss/sum: 0 0 0
used/not used/entry size/cache size: 0 8388608 32 256MB
uniqueHash elements/entry size/size: 67108864 4 256MB
0 66999371
1 107044
2 2349
3 96
4 2
5 2
6 0
7 0
8 0
9 0
>= 10 0

Total processing time: 0m20.901sec


BK_STOP 1678387994350

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

check for maximal unmarked siphon
ok
check for constant places
SpeedPossibleVal_1
SpeedPossibleVal_2
SpeedPossibleVal_3
SpeedPossibleVal_4
SpeedPossibleVal_5
SpeedPossibleVal_6
SpeedPossibleVal_7
SpeedPossibleVal_8
SpeedPossibleVal_9
SpeedPossibleVal_10
AltitudePossibleVal_1
AltitudePossibleVal_2
AltitudePossibleVal_3
AltitudePossibleVal_4
AltitudePossibleVal_5
AltitudePossibleVal_6
AltitudePossibleVal_7
AltitudePossibleVal_8
AltitudePossibleVal_9
AltitudePossibleVal_10
AltitudePossibleVal_11
AltitudePossibleVal_12
AltitudePossibleVal_13
AltitudePossibleVal_14
AltitudePossibleVal_15
AltitudePossibleVal_16
AltitudePossibleVal_17
AltitudePossibleVal_18
AltitudePossibleVal_19
AltitudePossibleVal_20
WeightPossibleVal_on
WeightPossibleVal_off
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 0.000sec


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:976 (11)

iterations count:91 (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:779 (8), effective:21 (0)

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

iterations count:94 (1), effective:1 (0)

iterations count:198 (2), effective:5 (0)

iterations count:198 (2), effective:5 (0)

iterations count:198 (2), effective:5 (0)

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

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

iterations count:672 (7), effective:17 (0)

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

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:976 (11)

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

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

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

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

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

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-PT-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-PT-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-oct2-167813588400241"
echo "====================================================================="
echo
echo "--------------------"
echo "preparation of the directory to be used:"

tar xzf /home/mcc/BenchKit/INPUTS/AirplaneLD-PT-0010.tgz
mv AirplaneLD-PT-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 ;